Start testing: Feb 18 12:38 CET ---------------------------------------------------------- 1/137 Testing: test_AerodynamicMomentAndAerodynamicForce 1/137 Test: test_AerodynamicMomentAndAerodynamicForce Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_AerodynamicMomentAndAerodynamicForce" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics "test_AerodynamicMomentAndAerodynamicForce" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 3 test cases... Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth 3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle 12, Rotation matrix from inertial frame to body frame of Vehicle 21, Rotation matrix from inertial frame to corotating frame of Vehicle 30, Rotation matrix from inertial frame to trajectory frame of Vehicle 39, Airspeed-based velocity of Vehicle 42, Single acceleration in inertial frame of type thrust , acting on Vehicle *** No errors detected Test time = 4.86 sec ---------------------------------------------------------- Test Passed. "test_AerodynamicMomentAndAerodynamicForce" end time: Feb 18 12:38 CET "test_AerodynamicMomentAndAerodynamicForce" time elapsed: 00:00:04 ---------------------------------------------------------- 2/137 Testing: test_AerodynamicsNamespace 2/137 Test: test_AerodynamicsNamespace Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_AerodynamicsNamespace" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics "test_AerodynamicsNamespace" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_AerodynamicsNamespace" end time: Feb 18 12:38 CET "test_AerodynamicsNamespace" time elapsed: 00:00:00 ---------------------------------------------------------- 3/137 Testing: test_AerodynamicCoefficientGenerator 3/137 Test: test_AerodynamicCoefficientGenerator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_AerodynamicCoefficientGenerator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics "test_AerodynamicCoefficientGenerator" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.03 sec ---------------------------------------------------------- Test Passed. "test_AerodynamicCoefficientGenerator" end time: Feb 18 12:38 CET "test_AerodynamicCoefficientGenerator" time elapsed: 00:00:00 ---------------------------------------------------------- 4/137 Testing: test_ExponentialAtmosphere 4/137 Test: test_ExponentialAtmosphere Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_ExponentialAtmosphere" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics "test_ExponentialAtmosphere" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_ExponentialAtmosphere" end time: Feb 18 12:38 CET "test_ExponentialAtmosphere" time elapsed: 00:00:00 ---------------------------------------------------------- 5/137 Testing: test_TabulatedAtmosphere 5/137 Test: test_TabulatedAtmosphere Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_TabulatedAtmosphere" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics "test_TabulatedAtmosphere" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 5 test cases... *** No errors detected Test time = 0.06 sec ---------------------------------------------------------- Test Passed. "test_TabulatedAtmosphere" end time: Feb 18 12:38 CET "test_TabulatedAtmosphere" time elapsed: 00:00:00 ---------------------------------------------------------- 6/137 Testing: test_TabulatedAerodynamicCoefficients 6/137 Test: test_TabulatedAerodynamicCoefficients Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_TabulatedAerodynamicCoefficients" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics "test_TabulatedAerodynamicCoefficients" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 2.27 sec ---------------------------------------------------------- Test Passed. "test_TabulatedAerodynamicCoefficients" end time: Feb 18 12:38 CET "test_TabulatedAerodynamicCoefficients" time elapsed: 00:00:02 ---------------------------------------------------------- 7/137 Testing: test_HeatTransfer 7/137 Test: test_HeatTransfer Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_HeatTransfer" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics "test_HeatTransfer" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 3 test cases... *** No errors detected Test time = 0.02 sec ---------------------------------------------------------- Test Passed. "test_HeatTransfer" end time: Feb 18 12:38 CET "test_HeatTransfer" time elapsed: 00:00:00 ---------------------------------------------------------- 8/137 Testing: test_ControlSurfaceIncrements 8/137 Test: test_ControlSurfaceIncrements Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_ControlSurfaceIncrements" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics "test_ControlSurfaceIncrements" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 2 test cases... Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Body orientation angle angle of attack of Apollo 2, Body orientation angle sideslip angle of Apollo 3, Control Surface Deflectionof Apollo w.r.t. TestSurface 4, Aerodynamic moment coefficients of Apollo 7, Aerodynamic force coefficients of Apollo *** No errors detected Test time = 0.50 sec ---------------------------------------------------------- Test Passed. "test_ControlSurfaceIncrements" end time: Feb 18 12:38 CET "test_ControlSurfaceIncrements" time elapsed: 00:00:00 ---------------------------------------------------------- 9/137 Testing: test_AerodynamicCoefficientsFromFile 9/137 Test: test_AerodynamicCoefficientsFromFile Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_AerodynamicCoefficientsFromFile" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics "test_AerodynamicCoefficientsFromFile" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of SpacePlane 1, Body orientation angle angle of attack of SpacePlane 2, Body orientation angle sideslip angle of SpacePlane 3, Body orientation angle bank angle of SpacePlane 4, Aerodynamic moment coefficients of SpacePlane 7, Aerodynamic force coefficients of SpacePlane Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of SpacePlane 1, Body orientation angle angle of attack of SpacePlane 2, Body orientation angle sideslip angle of SpacePlane 3, Body orientation angle bank angle of SpacePlane 4, Control Surface Deflectionof SpacePlane w.r.t. TestSurface 5, Aerodynamic moment coefficients of SpacePlane 8, Aerodynamic force coefficients of SpacePlane Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of SpacePlane 1, Body orientation angle angle of attack of SpacePlane 2, Body orientation angle sideslip angle of SpacePlane 3, Body orientation angle bank angle of SpacePlane 4, Control Surface Deflectionof SpacePlane w.r.t. TestSurface 5, Aerodynamic moment coefficients of SpacePlane 8, Aerodynamic force coefficients of SpacePlane *** No errors detected Test time = 0.42 sec ---------------------------------------------------------- Test Passed. "test_AerodynamicCoefficientsFromFile" end time: Feb 18 12:38 CET "test_AerodynamicCoefficientsFromFile" time elapsed: 00:00:00 ---------------------------------------------------------- 10/137 Testing: test_NRLMSISE00Atmosphere 10/137 Test: test_NRLMSISE00Atmosphere Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_NRLMSISE00Atmosphere" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics "test_NRLMSISE00Atmosphere" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 24 test cases... *** No errors detected Test time = 0.03 sec ---------------------------------------------------------- Test Passed. "test_NRLMSISE00Atmosphere" end time: Feb 18 12:38 CET "test_NRLMSISE00Atmosphere" time elapsed: 00:00:00 ---------------------------------------------------------- 11/137 Testing: test_AstrodynamicsFunctions 11/137 Test: test_AstrodynamicsFunctions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_AstrodynamicsFunctions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_AstrodynamicsFunctions" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 5 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_AstrodynamicsFunctions" end time: Feb 18 12:38 CET "test_AstrodynamicsFunctions" time elapsed: 00:00:00 ---------------------------------------------------------- 12/137 Testing: test_OrbitalElementConversions 12/137 Test: test_OrbitalElementConversions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_OrbitalElementConversions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_OrbitalElementConversions" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 11 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_OrbitalElementConversions" end time: Feb 18 12:38 CET "test_OrbitalElementConversions" time elapsed: 00:00:00 ---------------------------------------------------------- 13/137 Testing: test_PhysicalConstants 13/137 Test: test_PhysicalConstants Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_PhysicalConstants" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_PhysicalConstants" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_PhysicalConstants" end time: Feb 18 12:38 CET "test_PhysicalConstants" time elapsed: 00:00:00 ---------------------------------------------------------- 14/137 Testing: test_UnitConversions 14/137 Test: test_UnitConversions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_UnitConversions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_UnitConversions" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 14 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_UnitConversions" end time: Feb 18 12:38 CET "test_UnitConversions" time elapsed: 00:00:00 ---------------------------------------------------------- 15/137 Testing: test_MeanToEccentricAnomalyConversion 15/137 Test: test_MeanToEccentricAnomalyConversion Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MeanToEccentricAnomalyConversion" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_MeanToEccentricAnomalyConversion" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 7 test cases... *** No errors detected Test time = 1.29 sec ---------------------------------------------------------- Test Passed. "test_MeanToEccentricAnomalyConversion" end time: Feb 18 12:38 CET "test_MeanToEccentricAnomalyConversion" time elapsed: 00:00:01 ---------------------------------------------------------- 16/137 Testing: test_MeanToHyperbolicEccentricAnomalyConversion 16/137 Test: test_MeanToHyperbolicEccentricAnomalyConversion Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MeanToHyperbolicEccentricAnomalyConversion" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_MeanToHyperbolicEccentricAnomalyConversion" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 5 test cases... *** No errors detected Test time = 1.96 sec ---------------------------------------------------------- Test Passed. "test_MeanToHyperbolicEccentricAnomalyConversion" end time: Feb 18 12:38 CET "test_MeanToHyperbolicEccentricAnomalyConversion" time elapsed: 00:00:01 ---------------------------------------------------------- 17/137 Testing: test_KeplerPropagator 17/137 Test: test_KeplerPropagator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_KeplerPropagator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_KeplerPropagator" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 6 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_KeplerPropagator" end time: Feb 18 12:38 CET "test_KeplerPropagator" time elapsed: 00:00:00 ---------------------------------------------------------- 18/137 Testing: test_AccelerationModel 18/137 Test: test_AccelerationModel Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_AccelerationModel" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_AccelerationModel" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 3 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_AccelerationModel" end time: Feb 18 12:38 CET "test_AccelerationModel" time elapsed: 00:00:00 ---------------------------------------------------------- 19/137 Testing: test_ClohessyWiltshirePropagator 19/137 Test: test_ClohessyWiltshirePropagator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_ClohessyWiltshirePropagator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_ClohessyWiltshirePropagator" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_ClohessyWiltshirePropagator" end time: Feb 18 12:38 CET "test_ClohessyWiltshirePropagator" time elapsed: 00:00:00 ---------------------------------------------------------- 20/137 Testing: test_MissionGeometry 20/137 Test: test_MissionGeometry Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MissionGeometry" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_MissionGeometry" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 6 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_MissionGeometry" end time: Feb 18 12:38 CET "test_MissionGeometry" time elapsed: 00:00:00 ---------------------------------------------------------- 21/137 Testing: test_TimeConversions 21/137 Test: test_TimeConversions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_TimeConversions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_TimeConversions" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 5 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_TimeConversions" end time: Feb 18 12:38 CET "test_TimeConversions" time elapsed: 00:00:00 ---------------------------------------------------------- 22/137 Testing: test_CelestialBodyConstants 22/137 Test: test_CelestialBodyConstants Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_CelestialBodyConstants" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_CelestialBodyConstants" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_CelestialBodyConstants" end time: Feb 18 12:38 CET "test_CelestialBodyConstants" time elapsed: 00:00:00 ---------------------------------------------------------- 23/137 Testing: test_ModifiedEquinoctialElementConversions 23/137 Test: test_ModifiedEquinoctialElementConversions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_ModifiedEquinoctialElementConversions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_ModifiedEquinoctialElementConversions" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_ModifiedEquinoctialElementConversions" end time: Feb 18 12:38 CET "test_ModifiedEquinoctialElementConversions" time elapsed: 00:00:00 ---------------------------------------------------------- 24/137 Testing: test_GeodeticCoordinateConversions 24/137 Test: test_GeodeticCoordinateConversions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_GeodeticCoordinateConversions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_GeodeticCoordinateConversions" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_GeodeticCoordinateConversions" end time: Feb 18 12:38 CET "test_GeodeticCoordinateConversions" time elapsed: 00:00:00 ---------------------------------------------------------- 25/137 Testing: test_StateElementConversions 25/137 Test: test_StateElementConversions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_StateElementConversions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_StateElementConversions" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_StateElementConversions" end time: Feb 18 12:38 CET "test_StateElementConversions" time elapsed: 00:00:00 ---------------------------------------------------------- 26/137 Testing: test_SphericalOrbitalStateConversions 26/137 Test: test_SphericalOrbitalStateConversions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_SphericalOrbitalStateConversions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_SphericalOrbitalStateConversions" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_SphericalOrbitalStateConversions" end time: Feb 18 12:38 CET "test_SphericalOrbitalStateConversions" time elapsed: 00:00:00 ---------------------------------------------------------- 27/137 Testing: test_BodyShapeModels 27/137 Test: test_BodyShapeModels Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_BodyShapeModels" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_BodyShapeModels" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_BodyShapeModels" end time: Feb 18 12:38 CET "test_BodyShapeModels" time elapsed: 00:00:00 ---------------------------------------------------------- 28/137 Testing: test_UnifiedStateModelElementConversions 28/137 Test: test_UnifiedStateModelElementConversions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_UnifiedStateModelElementConversions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics "test_UnifiedStateModelElementConversions" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_UnifiedStateModelElementConversions" end time: Feb 18 12:38 CET "test_UnifiedStateModelElementConversions" time elapsed: 00:00:00 ---------------------------------------------------------- 29/137 Testing: test_CannonBallRadiationPressureAccelerationAndForce 29/137 Test: test_CannonBallRadiationPressureAccelerationAndForce Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_CannonBallRadiationPressureAccelerationAndForce" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/ElectroMagnetism "test_CannonBallRadiationPressureAccelerationAndForce" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 9 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_CannonBallRadiationPressureAccelerationAndForce" end time: Feb 18 12:38 CET "test_CannonBallRadiationPressureAccelerationAndForce" time elapsed: 00:00:00 ---------------------------------------------------------- 30/137 Testing: test_LorentzStaticMagneticAccelerationAndForce 30/137 Test: test_LorentzStaticMagneticAccelerationAndForce Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_LorentzStaticMagneticAccelerationAndForce" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/ElectroMagnetism "test_LorentzStaticMagneticAccelerationAndForce" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 5 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_LorentzStaticMagneticAccelerationAndForce" end time: Feb 18 12:38 CET "test_LorentzStaticMagneticAccelerationAndForce" time elapsed: 00:00:00 ---------------------------------------------------------- 31/137 Testing: test_RadiationPressureInterface 31/137 Test: test_RadiationPressureInterface Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_RadiationPressureInterface" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/ElectroMagnetism "test_RadiationPressureInterface" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_RadiationPressureInterface" end time: Feb 18 12:38 CET "test_RadiationPressureInterface" time elapsed: 00:00:00 ---------------------------------------------------------- 32/137 Testing: test_ApproximatePlanetPositions 32/137 Test: test_ApproximatePlanetPositions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_ApproximatePlanetPositions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides "test_ApproximatePlanetPositions" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_ApproximatePlanetPositions" end time: Feb 18 12:38 CET "test_ApproximatePlanetPositions" time elapsed: 00:00:00 ---------------------------------------------------------- 33/137 Testing: test_TabulatedEphemeris 33/137 Test: test_TabulatedEphemeris Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_TabulatedEphemeris" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides "test_TabulatedEphemeris" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.07 sec ---------------------------------------------------------- Test Passed. "test_TabulatedEphemeris" end time: Feb 18 12:38 CET "test_TabulatedEphemeris" time elapsed: 00:00:00 ---------------------------------------------------------- 34/137 Testing: test_CartesianStateExtractor 34/137 Test: test_CartesianStateExtractor Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_CartesianStateExtractor" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides "test_CartesianStateExtractor" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 7 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_CartesianStateExtractor" end time: Feb 18 12:38 CET "test_CartesianStateExtractor" time elapsed: 00:00:00 ---------------------------------------------------------- 35/137 Testing: test_KeplerStateExtractor 35/137 Test: test_KeplerStateExtractor Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_KeplerStateExtractor" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides "test_KeplerStateExtractor" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 8 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_KeplerStateExtractor" end time: Feb 18 12:38 CET "test_KeplerStateExtractor" time elapsed: 00:00:00 ---------------------------------------------------------- 36/137 Testing: test_RotationalEphemeris 36/137 Test: test_RotationalEphemeris Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_RotationalEphemeris" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides "test_RotationalEphemeris" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_RotationalEphemeris" end time: Feb 18 12:38 CET "test_RotationalEphemeris" time elapsed: 00:00:00 ---------------------------------------------------------- 37/137 Testing: test_SimpleRotationalEphemeris 37/137 Test: test_SimpleRotationalEphemeris Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_SimpleRotationalEphemeris" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides "test_SimpleRotationalEphemeris" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_SimpleRotationalEphemeris" end time: Feb 18 12:38 CET "test_SimpleRotationalEphemeris" time elapsed: 00:00:00 ---------------------------------------------------------- 38/137 Testing: test_FrameManager 38/137 Test: test_FrameManager Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_FrameManager" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides "test_FrameManager" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.10 sec ---------------------------------------------------------- Test Passed. "test_FrameManager" end time: Feb 18 12:38 CET "test_FrameManager" time elapsed: 00:00:00 ---------------------------------------------------------- 39/137 Testing: test_CompositeEphemeris 39/137 Test: test_CompositeEphemeris Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_CompositeEphemeris" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides "test_CompositeEphemeris" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.16 sec ---------------------------------------------------------- Test Passed. "test_CompositeEphemeris" end time: Feb 18 12:38 CET "test_CompositeEphemeris" time elapsed: 00:00:00 ---------------------------------------------------------- 40/137 Testing: test_KeplerEphemeris 40/137 Test: test_KeplerEphemeris Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_KeplerEphemeris" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides "test_KeplerEphemeris" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_KeplerEphemeris" end time: Feb 18 12:38 CET "test_KeplerEphemeris" time elapsed: 00:00:00 ---------------------------------------------------------- 41/137 Testing: test_SphericalHarmonicsGravityField 41/137 Test: test_SphericalHarmonicsGravityField Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_SphericalHarmonicsGravityField" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation "test_SphericalHarmonicsGravityField" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_SphericalHarmonicsGravityField" end time: Feb 18 12:38 CET "test_SphericalHarmonicsGravityField" time elapsed: 00:00:00 ---------------------------------------------------------- 42/137 Testing: test_GravitationalForce 42/137 Test: test_GravitationalForce Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_GravitationalForce" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation "test_GravitationalForce" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_GravitationalForce" end time: Feb 18 12:38 CET "test_GravitationalForce" time elapsed: 00:00:00 ---------------------------------------------------------- 43/137 Testing: test_CentralAndZonalGravityModel 43/137 Test: test_CentralAndZonalGravityModel Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_CentralAndZonalGravityModel" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation "test_CentralAndZonalGravityModel" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 5 test cases... *** No errors detected Test time = 0.02 sec ---------------------------------------------------------- Test Passed. "test_CentralAndZonalGravityModel" end time: Feb 18 12:38 CET "test_CentralAndZonalGravityModel" time elapsed: 00:00:00 ---------------------------------------------------------- 44/137 Testing: test_UnitConversionsCircularRestrictedThreeBodyProblem 44/137 Test: test_UnitConversionsCircularRestrictedThreeBodyProblem Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_UnitConversionsCircularRestrictedThreeBodyProblem" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation "test_UnitConversionsCircularRestrictedThreeBodyProblem" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_UnitConversionsCircularRestrictedThreeBodyProblem" end time: Feb 18 12:38 CET "test_UnitConversionsCircularRestrictedThreeBodyProblem" time elapsed: 00:00:00 ---------------------------------------------------------- 45/137 Testing: test_JacobiEnergy 45/137 Test: test_JacobiEnergy Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_JacobiEnergy" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation "test_JacobiEnergy" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_JacobiEnergy" end time: Feb 18 12:38 CET "test_JacobiEnergy" time elapsed: 00:00:00 ---------------------------------------------------------- 46/137 Testing: test_LibrationPoints 46/137 Test: test_LibrationPoints Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_LibrationPoints" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation "test_LibrationPoints" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 6 test cases... *** No errors detected Test time = 0.02 sec ---------------------------------------------------------- Test Passed. "test_LibrationPoints" end time: Feb 18 12:38 CET "test_LibrationPoints" time elapsed: 00:00:00 ---------------------------------------------------------- 47/137 Testing: test_StateDerivativeRestrictedThreeBodyProblem 47/137 Test: test_StateDerivativeRestrictedThreeBodyProblem Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_StateDerivativeRestrictedThreeBodyProblem" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation "test_StateDerivativeRestrictedThreeBodyProblem" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_StateDerivativeRestrictedThreeBodyProblem" end time: Feb 18 12:38 CET "test_StateDerivativeRestrictedThreeBodyProblem" time elapsed: 00:00:00 ---------------------------------------------------------- 48/137 Testing: test_SphericalHarmonicsGravityModel 48/137 Test: test_SphericalHarmonicsGravityModel Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_SphericalHarmonicsGravityModel" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation "test_SphericalHarmonicsGravityModel" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 5 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_SphericalHarmonicsGravityModel" end time: Feb 18 12:38 CET "test_SphericalHarmonicsGravityModel" time elapsed: 00:00:00 ---------------------------------------------------------- 49/137 Testing: test_ThirdBodyPerturbation 49/137 Test: test_ThirdBodyPerturbation Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_ThirdBodyPerturbation" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation "test_ThirdBodyPerturbation" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_ThirdBodyPerturbation" end time: Feb 18 12:38 CET "test_ThirdBodyPerturbation" time elapsed: 00:00:00 ---------------------------------------------------------- 50/137 Testing: test_TriAxialEllipsoidGravity 50/137 Test: test_TriAxialEllipsoidGravity Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_TriAxialEllipsoidGravity" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation "test_TriAxialEllipsoidGravity" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_TriAxialEllipsoidGravity" end time: Feb 18 12:38 CET "test_TriAxialEllipsoidGravity" time elapsed: 00:00:00 ---------------------------------------------------------- 51/137 Testing: test_GravityFieldVariations 51/137 Test: test_GravityFieldVariations Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_GravityFieldVariations" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation "test_GravityFieldVariations" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.09 sec ---------------------------------------------------------- Test Passed. "test_GravityFieldVariations" end time: Feb 18 12:38 CET "test_GravityFieldVariations" time elapsed: 00:00:00 ---------------------------------------------------------- 52/137 Testing: test_MutualSphericalHarmonicsGravityModel 52/137 Test: test_MutualSphericalHarmonicsGravityModel Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MutualSphericalHarmonicsGravityModel" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation "test_MutualSphericalHarmonicsGravityModel" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.11 sec ---------------------------------------------------------- Test Passed. "test_MutualSphericalHarmonicsGravityModel" end time: Feb 18 12:38 CET "test_MutualSphericalHarmonicsGravityModel" time elapsed: 00:00:00 ---------------------------------------------------------- 53/137 Testing: test_EscapeAndCapture 53/137 Test: test_EscapeAndCapture Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_EscapeAndCapture" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments "test_EscapeAndCapture" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 3 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_EscapeAndCapture" end time: Feb 18 12:38 CET "test_EscapeAndCapture" time elapsed: 00:00:00 ---------------------------------------------------------- 54/137 Testing: test_GravityAssist 54/137 Test: test_GravityAssist Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_GravityAssist" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments "test_GravityAssist" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 14 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_GravityAssist" end time: Feb 18 12:38 CET "test_GravityAssist" time elapsed: 00:00:00 ---------------------------------------------------------- 55/137 Testing: test_LambertTargeterIzzo 55/137 Test: test_LambertTargeterIzzo Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_LambertTargeterIzzo" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments "test_LambertTargeterIzzo" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_LambertTargeterIzzo" end time: Feb 18 12:38 CET "test_LambertTargeterIzzo" time elapsed: 00:00:00 ---------------------------------------------------------- 56/137 Testing: test_LambertTargeterGooding 56/137 Test: test_LambertTargeterGooding Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_LambertTargeterGooding" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments "test_LambertTargeterGooding" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_LambertTargeterGooding" end time: Feb 18 12:38 CET "test_LambertTargeterGooding" time elapsed: 00:00:00 ---------------------------------------------------------- 57/137 Testing: test_LambertTargeter 57/137 Test: test_LambertTargeter Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_LambertTargeter" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments "test_LambertTargeter" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_LambertTargeter" end time: Feb 18 12:38 CET "test_LambertTargeter" time elapsed: 00:00:00 ---------------------------------------------------------- 58/137 Testing: test_LambertRoutines 58/137 Test: test_LambertRoutines Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_LambertRoutines" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments "test_LambertRoutines" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 13 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_LambertRoutines" end time: Feb 18 12:38 CET "test_LambertRoutines" time elapsed: 00:00:00 ---------------------------------------------------------- 59/137 Testing: test_ZeroRevolutionLambertTargeterIzzo 59/137 Test: test_ZeroRevolutionLambertTargeterIzzo Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_ZeroRevolutionLambertTargeterIzzo" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments "test_ZeroRevolutionLambertTargeterIzzo" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_ZeroRevolutionLambertTargeterIzzo" end time: Feb 18 12:38 CET "test_ZeroRevolutionLambertTargeterIzzo" time elapsed: 00:00:00 ---------------------------------------------------------- 60/137 Testing: test_MultiRevolutionLambertTargeterIzzo 60/137 Test: test_MultiRevolutionLambertTargeterIzzo Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MultiRevolutionLambertTargeterIzzo" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments "test_MultiRevolutionLambertTargeterIzzo" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 3 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_MultiRevolutionLambertTargeterIzzo" end time: Feb 18 12:38 CET "test_MultiRevolutionLambertTargeterIzzo" time elapsed: 00:00:00 ---------------------------------------------------------- 61/137 Testing: test_MathematicalShapeFunctions 61/137 Test: test_MathematicalShapeFunctions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MathematicalShapeFunctions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments "test_MathematicalShapeFunctions" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 3 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_MathematicalShapeFunctions" end time: Feb 18 12:38 CET "test_MathematicalShapeFunctions" time elapsed: 00:00:00 ---------------------------------------------------------- 62/137 Testing: test_ReferenceFrameTransformations 62/137 Test: test_ReferenceFrameTransformations Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_ReferenceFrameTransformations" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/ReferenceFrames "test_ReferenceFrameTransformations" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 10 test cases... *** No errors detected Test time = 0.04 sec ---------------------------------------------------------- Test Passed. "test_ReferenceFrameTransformations" end time: Feb 18 12:38 CET "test_ReferenceFrameTransformations" time elapsed: 00:00:00 ---------------------------------------------------------- 63/137 Testing: test_ApparentAccelerationModel 63/137 Test: test_ApparentAccelerationModel Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_ApparentAccelerationModel" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/ReferenceFrames "test_ApparentAccelerationModel" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 5 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_ApparentAccelerationModel" end time: Feb 18 12:38 CET "test_ApparentAccelerationModel" time elapsed: 00:00:00 ---------------------------------------------------------- 64/137 Testing: test_AerodynamicAngleCalculator 64/137 Test: test_AerodynamicAngleCalculator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_AerodynamicAngleCalculator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/ReferenceFrames "test_AerodynamicAngleCalculator" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_AerodynamicAngleCalculator" end time: Feb 18 12:38 CET "test_AerodynamicAngleCalculator" time elapsed: 00:00:00 ---------------------------------------------------------- 65/137 Testing: test_LightTime 65/137 Test: test_LightTime Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_LightTime" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/ObservationModels "test_LightTime" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.07 sec ---------------------------------------------------------- Test Passed. "test_LightTime" end time: Feb 18 12:38 CET "test_LightTime" time elapsed: 00:00:00 ---------------------------------------------------------- 66/137 Testing: test_AngularPositionModel 66/137 Test: test_AngularPositionModel Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_AngularPositionModel" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/ObservationModels "test_AngularPositionModel" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... Warning, position of Mars taken as barycenter of that body's planetary system. *** No errors detected Test time = 0.12 sec ---------------------------------------------------------- Test Passed. "test_AngularPositionModel" end time: Feb 18 12:38 CET "test_AngularPositionModel" time elapsed: 00:00:00 ---------------------------------------------------------- 67/137 Testing: test_OneWayRangeModel 67/137 Test: test_OneWayRangeModel Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_OneWayRangeModel" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/ObservationModels "test_OneWayRangeModel" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... Warning, position of Mars taken as barycenter of that body's planetary system. *** No errors detected Test time = 0.13 sec ---------------------------------------------------------- Test Passed. "test_OneWayRangeModel" end time: Feb 18 12:38 CET "test_OneWayRangeModel" time elapsed: 00:00:00 ---------------------------------------------------------- 68/137 Testing: test_PositionObservationModel 68/137 Test: test_PositionObservationModel Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_PositionObservationModel" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/ObservationModels "test_PositionObservationModel" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.12 sec ---------------------------------------------------------- Test Passed. "test_PositionObservationModel" end time: Feb 18 12:38 CET "test_PositionObservationModel" time elapsed: 00:00:00 ---------------------------------------------------------- 69/137 Testing: test_AccelerationPartials 69/137 Test: test_AccelerationPartials Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_AccelerationPartials" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/OrbitDetermination/AccelerationPartials "test_AccelerationPartials" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 3 test cases... *** No errors detected Test time = 0.04 sec ---------------------------------------------------------- Test Passed. "test_AccelerationPartials" end time: Feb 18 12:38 CET "test_AccelerationPartials" time elapsed: 00:00:00 ---------------------------------------------------------- 70/137 Testing: test_SphericalHarmonicPartials 70/137 Test: test_SphericalHarmonicPartials Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_SphericalHarmonicPartials" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/OrbitDetermination/AccelerationPartials "test_SphericalHarmonicPartials" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.10 sec ---------------------------------------------------------- Test Passed. "test_SphericalHarmonicPartials" end time: Feb 18 12:38 CET "test_SphericalHarmonicPartials" time elapsed: 00:00:00 ---------------------------------------------------------- 71/137 Testing: test_RotationMatrixPartials 71/137 Test: test_RotationMatrixPartials Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_RotationMatrixPartials" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/OrbitDetermination/ObservationPartials "test_RotationMatrixPartials" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.10 sec ---------------------------------------------------------- Test Passed. "test_RotationMatrixPartials" end time: Feb 18 12:38 CET "test_RotationMatrixPartials" time elapsed: 00:00:00 ---------------------------------------------------------- 72/137 Testing: test_CentralBodyData 72/137 Test: test_CentralBodyData Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_CentralBodyData" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators "test_CentralBodyData" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_CentralBodyData" end time: Feb 18 12:38 CET "test_CentralBodyData" time elapsed: 00:00:00 ---------------------------------------------------------- 73/137 Testing: test_CowellStateDerivative 73/137 Test: test_CowellStateDerivative Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_CowellStateDerivative" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators "test_CowellStateDerivative" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 2 test cases... Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision unknown location:0: fatal error in "testCowellPopagatorKeplerCompare": signal: SIGSEGV, si_code: 0 (memory access violation at address: 0x00000000) /Users/gigilaan/tudatBundle/tudat/Tudat/Astrodynamics/Propagators/UnitTests/unitTestCowellStateDerivative.cpp:479: last checkpoint *** 1 failure detected in test suite "Master Test Suite" Test time = 10.71 sec ---------------------------------------------------------- Test Failed. "test_CowellStateDerivative" end time: Feb 18 12:38 CET "test_CowellStateDerivative" time elapsed: 00:00:10 ---------------------------------------------------------- 74/137 Testing: test_EnckeStateDerivative 74/137 Test: test_EnckeStateDerivative Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_EnckeStateDerivative" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators "test_EnckeStateDerivative" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 3 test cases... Warning, position of Jupiter taken as barycenter of that body's planetary system. Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Jupiter taken as barycenter of that body's planetary system. Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Testint with eccentricity 0.8Testint with eccentricity 0.9Testint with eccentricity 0.95Testint with eccentricity 0.99 *** No errors detected Test time = 15.40 sec ---------------------------------------------------------- Test Passed. "test_EnckeStateDerivative" end time: Feb 18 12:38 CET "test_EnckeStateDerivative" time elapsed: 00:00:15 ---------------------------------------------------------- 75/137 Testing: test_SequentialVariationEquationIntegration 75/137 Test: test_SequentialVariationEquationIntegration Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_SequentialVariationEquationIntegration" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators "test_SequentialVariationEquationIntegration" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision *** No errors detected Test time = 9.86 sec ---------------------------------------------------------- Test Passed. "test_SequentialVariationEquationIntegration" end time: Feb 18 12:38 CET "test_SequentialVariationEquationIntegration" time elapsed: 00:00:09 ---------------------------------------------------------- 76/137 Testing: test_VariationalEquations 76/137 Test: test_VariationalEquations Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_VariationalEquations" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators "test_VariationalEquations" start time: Feb 18 12:38 CET Output: ---------------------------------------------------------- Running 1 test case... Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, position of Mars taken as barycenter of that body's planetary system. Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision *** No errors detected Test time = 30.88 sec ---------------------------------------------------------- Test Passed. "test_VariationalEquations" end time: Feb 18 12:39 CET "test_VariationalEquations" time elapsed: 00:00:30 ---------------------------------------------------------- 77/137 Testing: test_EnvironmentModelUpdater 77/137 Test: test_EnvironmentModelUpdater Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_EnvironmentModelUpdater" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators "test_EnvironmentModelUpdater" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... Warning, position of Mars taken as barycenter of that body's planetary system. *** No errors detected Test time = 0.32 sec ---------------------------------------------------------- Test Passed. "test_EnvironmentModelUpdater" end time: Feb 18 12:39 CET "test_EnvironmentModelUpdater" time elapsed: 00:00:00 ---------------------------------------------------------- 78/137 Testing: test_BodyMassPropagation 78/137 Test: test_BodyMassPropagation Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_BodyMassPropagation" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators "test_BodyMassPropagation" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.04 sec ---------------------------------------------------------- Test Passed. "test_BodyMassPropagation" end time: Feb 18 12:39 CET "test_BodyMassPropagation" time elapsed: 00:00:00 ---------------------------------------------------------- 79/137 Testing: test_MultiTypeStatePropagation 79/137 Test: test_MultiTypeStatePropagation Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MultiTypeStatePropagation" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators "test_MultiTypeStatePropagation" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision Warning, tabulated ephemeris is being reset using data at different precision *** No errors detected Test time = 0.88 sec ---------------------------------------------------------- Test Passed. "test_MultiTypeStatePropagation" end time: Feb 18 12:39 CET "test_MultiTypeStatePropagation" time elapsed: 00:00:00 ---------------------------------------------------------- 80/137 Testing: test_DependentVariableOutput 80/137 Test: test_DependentVariableOutput Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_DependentVariableOutput" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators "test_DependentVariableOutput" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Altitude of Apollo w.r.t. Earth 2, Relative distance of Apollo w.r.t. Earth 3, Relative speed of Apollo w.r.t. Earth 4, Single acceleration norm of type central gravity , acting on Apollo, exerted by Earth 5, Aerodynamic g-load of Apollo w.r.t. Earth 6, Stagnation-point heat flux of Apollo w.r.t. Earth 7, Local freestream temperature of Apollo w.r.t. Earth 8, Geodetic latitude of Apollo w.r.t. Earth 9, Density of Apollo w.r.t. Earth 10, Body orientation angle latitude angle of Apollo 11, Body orientation angle longitude angle of Apollo 12, Body orientation angle angle of attack of Apollo 13, Body orientation angle sideslip angle of Apollo 14, Body orientation angle bank angle of Apollo 15, Relative position of Apollo w.r.t. Earth 18, Relative velocity of Apollo w.r.t. Earth 21, Single acceleration in inertial frame of type central gravity , acting on Apollo, exerted by Earth 24, Total acceleration in inertial frame of Apollo 27, Aerodynamic moment coefficients of Apollo 30, Aerodynamic force coefficients of Apollo 33, Single acceleration in inertial frame of type aerodynamic , acting on Apollo, exerted by Earth Propagated Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Altitude of Apollo w.r.t. Earth 2, Relative distance of Apollo w.r.t. Earth 3, Relative speed of Apollo w.r.t. Earth 4, Single acceleration norm of type central gravity , acting on Apollo, exerted by Earth 5, Aerodynamic g-load of Apollo w.r.t. Earth 6, Stagnation-point heat flux of Apollo w.r.t. Earth 7, Local freestream temperature of Apollo w.r.t. Earth 8, Geodetic latitude of Apollo w.r.t. Earth 9, Density of Apollo w.r.t. Earth 10, Body orientation angle latitude angle of Apollo 11, Body orientation angle longitude angle of Apollo 12, Body orientation angle angle of attack of Apollo 13, Body orientation angle sideslip angle of Apollo 14, Body orientation angle bank angle of Apollo 15, Relative position of Apollo w.r.t. Earth 18, Relative velocity of Apollo w.r.t. Earth 21, Single acceleration in inertial frame of type central gravity , acting on Apollo, exerted by Earth 24, Total acceleration in inertial frame of Apollo 27, Aerodynamic moment coefficients of Apollo 30, Aerodynamic force coefficients of Apollo 33, Single acceleration in inertial frame of type aerodynamic , acting on Apollo, exerted by Earth Propagated Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Altitude of Apollo w.r.t. Earth 2, Relative distance of Apollo w.r.t. Earth 3, Relative speed of Apollo w.r.t. Earth 4, Single acceleration norm of type central gravity , acting on Apollo, exerted by Earth 5, Aerodynamic g-load of Apollo w.r.t. Earth 6, Stagnation-point heat flux of Apollo w.r.t. Earth 7, Local freestream temperature of Apollo w.r.t. Earth 8, Geodetic latitude of Apollo w.r.t. Earth 9, Density of Apollo w.r.t. Earth 10, Body orientation angle latitude angle of Apollo 11, Body orientation angle longitude angle of Apollo 12, Body orientation angle angle of attack of Apollo 13, Body orientation angle sideslip angle of Apollo 14, Body orientation angle bank angle of Apollo 15, Relative position of Apollo w.r.t. Earth 18, Relative velocity of Apollo w.r.t. Earth 21, Single acceleration in inertial frame of type central gravity , acting on Apollo, exerted by Earth 24, Total acceleration in inertial frame of Apollo 27, Aerodynamic moment coefficients of Apollo 30, Aerodynamic force coefficients of Apollo 33, Single acceleration in inertial frame of type aerodynamic , acting on Apollo, exerted by Earth Propagated Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Altitude of Apollo w.r.t. Earth 2, Relative distance of Apollo w.r.t. Earth 3, Relative speed of Apollo w.r.t. Earth 4, Single acceleration norm of type central gravity , acting on Apollo, exerted by Earth 5, Aerodynamic g-load of Apollo w.r.t. Earth 6, Stagnation-point heat flux of Apollo w.r.t. Earth 7, Local freestream temperature of Apollo w.r.t. Earth 8, Geodetic latitude of Apollo w.r.t. Earth 9, Density of Apollo w.r.t. Earth 10, Body orientation angle latitude angle of Apollo 11, Body orientation angle longitude angle of Apollo 12, Body orientation angle angle of attack of Apollo 13, Body orientation angle sideslip angle of Apollo 14, Body orientation angle bank angle of Apollo 15, Relative position of Apollo w.r.t. Earth 18, Relative velocity of Apollo w.r.t. Earth 21, Single acceleration in inertial frame of type central gravity , acting on Apollo, exerted by Earth 24, Total acceleration in inertial frame of Apollo 27, Aerodynamic moment coefficients of Apollo 30, Aerodynamic force coefficients of Apollo 33, Single acceleration in inertial frame of type aerodynamic , acting on Apollo, exerted by Earth Propagated *** No errors detected Test time = 10.78 sec ---------------------------------------------------------- Test Passed. "test_DependentVariableOutput" end time: Feb 18 12:39 CET "test_DependentVariableOutput" time elapsed: 00:00:10 ---------------------------------------------------------- 81/137 Testing: test_StoppingConditions 81/137 Test: test_StoppingConditions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_StoppingConditions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators "test_StoppingConditions" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 2.87 sec ---------------------------------------------------------- Test Passed. "test_StoppingConditions" end time: Feb 18 12:39 CET "test_StoppingConditions" time elapsed: 00:00:02 ---------------------------------------------------------- 82/137 Testing: test_CustomStatePropagation 82/137 Test: test_CustomStatePropagation Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_CustomStatePropagation" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators "test_CustomStatePropagation" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 5 test cases... Warning, tabulated ephemeris is being reset using data at different precision *** No errors detected Test time = 0.36 sec ---------------------------------------------------------- Test Passed. "test_CustomStatePropagation" end time: Feb 18 12:39 CET "test_CustomStatePropagation" time elapsed: 00:00:00 ---------------------------------------------------------- 83/137 Testing: test_ShapiroTimeDelay 83/137 Test: test_ShapiroTimeDelay Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_ShapiroTimeDelay" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Relativity "test_ShapiroTimeDelay" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_ShapiroTimeDelay" end time: Feb 18 12:39 CET "test_ShapiroTimeDelay" time elapsed: 00:00:00 ---------------------------------------------------------- 84/137 Testing: test_ThrustAcceleration 84/137 Test: test_ThrustAcceleration Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_ThrustAcceleration" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/Propulsion "test_ThrustAcceleration" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 8 test cases... Warning, cannot reset dependentOrientationCalculator, incompatible object already exists Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type thrust , acting on Vehicle Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Body orientation angle angle of attack of Apollo 2, Body orientation angle sideslip angle of Apollo 3, Body orientation angle bank angle of Apollo 4, Airspeed of Apollo w.r.t. Earth 5, Density of Apollo w.r.t. Earth 6, Rotation matrix from inertial frame to body frame of Apollo 15, Rotation matrix to body-fixed frame of Apollo 24, Single acceleration in inertial frame of type aerodynamic , acting on Apollo, exerted by Earth 27, Single acceleration in inertial frame of type thrust , acting on Apollo 30, Aerodynamic force coefficients of Apollo 33, Aerodynamic moment coefficients of Apollo 36, Rotation matrix from inertial frame to aerodynamic frame of Apollo 45, Rotation matrix from aerodynamic frame to body frame of Apollo Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Body orientation angle angle of attack of Apollo 2, Body orientation angle sideslip angle of Apollo 3, Body orientation angle bank angle of Apollo 4, Airspeed of Apollo w.r.t. Earth 5, Density of Apollo w.r.t. Earth 6, Rotation matrix from inertial frame to body frame of Apollo 15, Rotation matrix to body-fixed frame of Apollo 24, Single acceleration in inertial frame of type aerodynamic , acting on Apollo, exerted by Earth 27, Single acceleration in inertial frame of type thrust , acting on Apollo 30, Aerodynamic force coefficients of Apollo 33, Aerodynamic moment coefficients of Apollo 36, Rotation matrix from inertial frame to aerodynamic frame of Apollo 45, Rotation matrix from aerodynamic frame to body frame of Apollo Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type thrust , acting on Asterix 3, Relative position of Asterix w.r.t. Earth 6, Relative velocity of Asterix w.r.t. Earth 9, LVLH to inertial frame rotation matrixof Asterix w.r.t. Earth Warning, cannot reset dependentOrientationCalculator, incompatible object already exists Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration in inertial frame of type thrust , acting on Asterix 3, Relative position of Asterix w.r.t. Earth 6, Relative velocity of Asterix w.r.t. Earth 9, LVLH to inertial frame rotation matrixof Asterix w.r.t. Earth Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Airspeed of Apollo 2, Density of Apollo 3, Single acceleration norm of type thrust , acting on Apollo 4, Body mass rateof Apollo Warning, overriding existing angle of attack function in AerodynamicAngleCalculator Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Airspeed of Apollo 2, Density of Apollo 3, Single acceleration norm of type thrust , acting on Apollo 4, Body mass rateof Apollo Warning, overriding existing angle of attack function in AerodynamicAngleCalculator Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Airspeed of Apollo 2, Density of Apollo 3, Single acceleration norm of type thrust , acting on Apollo 4, Body mass rateof Apollo Warning, overriding existing angle of attack function in AerodynamicAngleCalculator Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Airspeed of Apollo 2, Density of Apollo 3, Single acceleration norm of type thrust , acting on Apollo 4, Body mass rateof Apollo Warning, overriding existing angle of attack function in AerodynamicAngleCalculator Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Airspeed of Apollo 2, Density of Apollo 3, Single acceleration norm of type thrust , acting on Apollo 4, Body mass rateof Apollo Warning, overriding existing angle of attack function in AerodynamicAngleCalculator Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Airspeed of Apollo 2, Density of Apollo 3, Single acceleration norm of type thrust , acting on Apollo 4, Body mass rateof Apollo Warning, overriding existing angle of attack function in AerodynamicAngleCalculator Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Airspeed of Apollo 2, Density of Apollo 3, Single acceleration norm of type thrust , acting on Apollo 4, Body mass rateof Apollo Warning, overriding existing angle of attack function in AerodynamicAngleCalculator Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Mach number of Apollo 1, Airspeed of Apollo 2, Density of Apollo 3, Single acceleration norm of type thrust , acting on Apollo 4, Body mass rateof Apollo Dependent variables being saved, output vectors contain: Vector entry, Vector contents 0, Single acceleration norm of type thrust , acting on Apollo *** No errors detected Test time = 6.47 sec ---------------------------------------------------------- Test Passed. "test_ThrustAcceleration" end time: Feb 18 12:39 CET "test_ThrustAcceleration" time elapsed: 00:00:06 ---------------------------------------------------------- 85/137 Testing: test_GroundStationState 85/137 Test: test_GroundStationState Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_GroundStationState" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Astrodynamics/GroundStations "test_GroundStationState" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.08 sec ---------------------------------------------------------- Test Passed. "test_GroundStationState" end time: Feb 18 12:39 CET "test_GroundStationState" time elapsed: 00:00:00 ---------------------------------------------------------- 86/137 Testing: test_TimeTypes 86/137 Test: test_TimeTypes Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_TimeTypes" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Basics "test_TimeTypes" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_TimeTypes" end time: Feb 18 12:39 CET "test_TimeTypes" time elapsed: 00:00:00 ---------------------------------------------------------- 87/137 Testing: test_MatrixTextFileReader 87/137 Test: test_MatrixTextFileReader Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MatrixTextFileReader" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_MatrixTextFileReader" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_MatrixTextFileReader" end time: Feb 18 12:39 CET "test_MatrixTextFileReader" time elapsed: 00:00:00 ---------------------------------------------------------- 88/137 Testing: test_StreamFilters 88/137 Test: test_StreamFilters Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_StreamFilters" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_StreamFilters" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 8 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_StreamFilters" end time: Feb 18 12:39 CET "test_StreamFilters" time elapsed: 00:00:00 ---------------------------------------------------------- 89/137 Testing: test_TwoLineElementsTextFileReader 89/137 Test: test_TwoLineElementsTextFileReader Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_TwoLineElementsTextFileReader" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_TwoLineElementsTextFileReader" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_TwoLineElementsTextFileReader" end time: Feb 18 12:39 CET "test_TwoLineElementsTextFileReader" time elapsed: 00:00:00 ---------------------------------------------------------- 90/137 Testing: test_BasicInputOutput 90/137 Test: test_BasicInputOutput Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_BasicInputOutput" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_BasicInputOutput" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 3 test cases... *** No errors detected Test time = 0.02 sec ---------------------------------------------------------- Test Passed. "test_BasicInputOutput" end time: Feb 18 12:39 CET "test_BasicInputOutput" time elapsed: 00:00:00 ---------------------------------------------------------- 91/137 Testing: test_ParsedDataVectorUtilities 91/137 Test: test_ParsedDataVectorUtilities Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_ParsedDataVectorUtilities" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_ParsedDataVectorUtilities" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 3 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_ParsedDataVectorUtilities" end time: Feb 18 12:39 CET "test_ParsedDataVectorUtilities" time elapsed: 00:00:00 ---------------------------------------------------------- 92/137 Testing: test_FieldValue 92/137 Test: test_FieldValue Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_FieldValue" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_FieldValue" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 5 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_FieldValue" end time: Feb 18 12:39 CET "test_FieldValue" time elapsed: 00:00:00 ---------------------------------------------------------- 93/137 Testing: test_TextParser 93/137 Test: test_TextParser Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_TextParser" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_TextParser" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_TextParser" end time: Feb 18 12:39 CET "test_TextParser" time elapsed: 00:00:00 ---------------------------------------------------------- 94/137 Testing: test_MissileDatcomReader 94/137 Test: test_MissileDatcomReader Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MissileDatcomReader" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_MissileDatcomReader" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_MissileDatcomReader" end time: Feb 18 12:39 CET "test_MissileDatcomReader" time elapsed: 00:00:00 ---------------------------------------------------------- 95/137 Testing: test_MissileDatcomData 95/137 Test: test_MissileDatcomData Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MissileDatcomData" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_MissileDatcomData" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.02 sec ---------------------------------------------------------- Test Passed. "test_MissileDatcomData" end time: Feb 18 12:39 CET "test_MissileDatcomData" time elapsed: 00:00:00 ---------------------------------------------------------- 96/137 Testing: test_DictionaryInputSystem 96/137 Test: test_DictionaryInputSystem Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_DictionaryInputSystem" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_DictionaryInputSystem" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_DictionaryInputSystem" end time: Feb 18 12:39 CET "test_DictionaryInputSystem" time elapsed: 00:00:00 ---------------------------------------------------------- 97/137 Testing: test_Extractor 97/137 Test: test_Extractor Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_Extractor" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_Extractor" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 3 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_Extractor" end time: Feb 18 12:39 CET "test_Extractor" time elapsed: 00:00:00 ---------------------------------------------------------- 98/137 Testing: test_FixedWidthParser 98/137 Test: test_FixedWidthParser Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_FixedWidthParser" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_FixedWidthParser" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_FixedWidthParser" end time: Feb 18 12:39 CET "test_FixedWidthParser" time elapsed: 00:00:00 ---------------------------------------------------------- 99/137 Testing: test_SeparatedParser 99/137 Test: test_SeparatedParser Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_SeparatedParser" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_SeparatedParser" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_SeparatedParser" end time: Feb 18 12:39 CET "test_SeparatedParser" time elapsed: 00:00:00 ---------------------------------------------------------- 100/137 Testing: test_LinearFieldTransform 100/137 Test: test_LinearFieldTransform Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_LinearFieldTransform" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_LinearFieldTransform" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_LinearFieldTransform" end time: Feb 18 12:39 CET "test_LinearFieldTransform" time elapsed: 00:00:00 ---------------------------------------------------------- 101/137 Testing: test_SolarActivityData 101/137 Test: test_SolarActivityData Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_SolarActivityData" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_SolarActivityData" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 1.45 sec ---------------------------------------------------------- Test Passed. "test_SolarActivityData" end time: Feb 18 12:39 CET "test_SolarActivityData" time elapsed: 00:00:01 ---------------------------------------------------------- 102/137 Testing: test_MultiArrayReader 102/137 Test: test_MultiArrayReader Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MultiArrayReader" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_MultiArrayReader" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_MultiArrayReader" end time: Feb 18 12:39 CET "test_MultiArrayReader" time elapsed: 00:00:00 ---------------------------------------------------------- 103/137 Testing: test_AerodynamicCoefficientReader 103/137 Test: test_AerodynamicCoefficientReader Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_AerodynamicCoefficientReader" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/InputOutput "test_AerodynamicCoefficientReader" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_AerodynamicCoefficientReader" end time: Feb 18 12:39 CET "test_AerodynamicCoefficientReader" time elapsed: 00:00:00 ---------------------------------------------------------- 104/137 Testing: test_MathematicalConstants 104/137 Test: test_MathematicalConstants Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MathematicalConstants" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics "test_MathematicalConstants" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 5 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_MathematicalConstants" end time: Feb 18 12:39 CET "test_MathematicalConstants" time elapsed: 00:00:00 ---------------------------------------------------------- 105/137 Testing: test_LinearAlgebra 105/137 Test: test_LinearAlgebra Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_LinearAlgebra" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics "test_LinearAlgebra" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_LinearAlgebra" end time: Feb 18 12:39 CET "test_LinearAlgebra" time elapsed: 00:00:00 ---------------------------------------------------------- 106/137 Testing: test_CoordinateConversions 106/137 Test: test_CoordinateConversions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_CoordinateConversions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics "test_CoordinateConversions" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 10 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_CoordinateConversions" end time: Feb 18 12:39 CET "test_CoordinateConversions" time elapsed: 00:00:00 ---------------------------------------------------------- 107/137 Testing: test_NearestNeighbourSearch 107/137 Test: test_NearestNeighbourSearch Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_NearestNeighbourSearch" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics "test_NearestNeighbourSearch" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_NearestNeighbourSearch" end time: Feb 18 12:39 CET "test_NearestNeighbourSearch" time elapsed: 00:00:00 ---------------------------------------------------------- 108/137 Testing: test_NumericalDerivative 108/137 Test: test_NumericalDerivative Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_NumericalDerivative" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics "test_NumericalDerivative" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.02 sec ---------------------------------------------------------- Test Passed. "test_NumericalDerivative" end time: Feb 18 12:39 CET "test_NumericalDerivative" time elapsed: 00:00:00 ---------------------------------------------------------- 109/137 Testing: test_LegendrePolynomials 109/137 Test: test_LegendrePolynomials Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_LegendrePolynomials" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics "test_LegendrePolynomials" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_LegendrePolynomials" end time: Feb 18 12:39 CET "test_LegendrePolynomials" time elapsed: 00:00:00 ---------------------------------------------------------- 110/137 Testing: test_SphericalHarmonics 110/137 Test: test_SphericalHarmonics Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_SphericalHarmonics" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics "test_SphericalHarmonics" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_SphericalHarmonics" end time: Feb 18 12:39 CET "test_SphericalHarmonics" time elapsed: 00:00:00 ---------------------------------------------------------- 111/137 Testing: test_RotationAboutArbitraryAxis 111/137 Test: test_RotationAboutArbitraryAxis Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_RotationAboutArbitraryAxis" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics "test_RotationAboutArbitraryAxis" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 5 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_RotationAboutArbitraryAxis" end time: Feb 18 12:39 CET "test_RotationAboutArbitraryAxis" time elapsed: 00:00:00 ---------------------------------------------------------- 112/137 Testing: test_LawgsSurfaceGeometry 112/137 Test: test_LawgsSurfaceGeometry Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_LawgsSurfaceGeometry" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/GeometricShapes "test_LawgsSurfaceGeometry" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_LawgsSurfaceGeometry" end time: Feb 18 12:39 CET "test_LawgsSurfaceGeometry" time elapsed: 00:00:00 ---------------------------------------------------------- 113/137 Testing: test_CubicSplineInterpolator 113/137 Test: test_CubicSplineInterpolator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_CubicSplineInterpolator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/Interpolators "test_CubicSplineInterpolator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.05 sec ---------------------------------------------------------- Test Passed. "test_CubicSplineInterpolator" end time: Feb 18 12:39 CET "test_CubicSplineInterpolator" time elapsed: 00:00:00 ---------------------------------------------------------- 114/137 Testing: test_HermiteCubicSplineInterpolator 114/137 Test: test_HermiteCubicSplineInterpolator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_HermiteCubicSplineInterpolator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/Interpolators "test_HermiteCubicSplineInterpolator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_HermiteCubicSplineInterpolator" end time: Feb 18 12:39 CET "test_HermiteCubicSplineInterpolator" time elapsed: 00:00:00 ---------------------------------------------------------- 115/137 Testing: test_LinearInterpolator 115/137 Test: test_LinearInterpolator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_LinearInterpolator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/Interpolators "test_LinearInterpolator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 3 test cases... *** No errors detected Test time = 0.04 sec ---------------------------------------------------------- Test Passed. "test_LinearInterpolator" end time: Feb 18 12:39 CET "test_LinearInterpolator" time elapsed: 00:00:00 ---------------------------------------------------------- 116/137 Testing: test_MultiLinearInterpolator 116/137 Test: test_MultiLinearInterpolator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MultiLinearInterpolator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/Interpolators "test_MultiLinearInterpolator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_MultiLinearInterpolator" end time: Feb 18 12:39 CET "test_MultiLinearInterpolator" time elapsed: 00:00:00 ---------------------------------------------------------- 117/137 Testing: test_LagrangeInterpolator 117/137 Test: test_LagrangeInterpolator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_LagrangeInterpolator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/Interpolators "test_LagrangeInterpolator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 3 test cases... *** No errors detected Test time = 0.02 sec ---------------------------------------------------------- Test Passed. "test_LagrangeInterpolator" end time: Feb 18 12:39 CET "test_LagrangeInterpolator" time elapsed: 00:00:00 ---------------------------------------------------------- 118/137 Testing: test_EulerIntegrator 118/137 Test: test_EulerIntegrator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_EulerIntegrator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators "test_EulerIntegrator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_EulerIntegrator" end time: Feb 18 12:39 CET "test_EulerIntegrator" time elapsed: 00:00:00 ---------------------------------------------------------- 119/137 Testing: test_NumericalIntegrator 119/137 Test: test_NumericalIntegrator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_NumericalIntegrator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators "test_NumericalIntegrator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_NumericalIntegrator" end time: Feb 18 12:39 CET "test_NumericalIntegrator" time elapsed: 00:00:00 ---------------------------------------------------------- 120/137 Testing: test_RungeKutta4Integrator 120/137 Test: test_RungeKutta4Integrator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_RungeKutta4Integrator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators "test_RungeKutta4Integrator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.02 sec ---------------------------------------------------------- Test Passed. "test_RungeKutta4Integrator" end time: Feb 18 12:39 CET "test_RungeKutta4Integrator" time elapsed: 00:00:00 ---------------------------------------------------------- 121/137 Testing: test_RungeKuttaVariableStepSizeIntegrator 121/137 Test: test_RungeKuttaVariableStepSizeIntegrator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_RungeKuttaVariableStepSizeIntegrator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators "test_RungeKuttaVariableStepSizeIntegrator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_RungeKuttaVariableStepSizeIntegrator" end time: Feb 18 12:39 CET "test_RungeKuttaVariableStepSizeIntegrator" time elapsed: 00:00:00 ---------------------------------------------------------- 122/137 Testing: test_RungeKuttaCoefficients 122/137 Test: test_RungeKuttaCoefficients Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_RungeKuttaCoefficients" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators "test_RungeKuttaCoefficients" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 3 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_RungeKuttaCoefficients" end time: Feb 18 12:39 CET "test_RungeKuttaCoefficients" time elapsed: 00:00:00 ---------------------------------------------------------- 123/137 Testing: test_RungeKuttaFehlberg45Integrator 123/137 Test: test_RungeKuttaFehlberg45Integrator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_RungeKuttaFehlberg45Integrator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators "test_RungeKuttaFehlberg45Integrator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.04 sec ---------------------------------------------------------- Test Passed. "test_RungeKuttaFehlberg45Integrator" end time: Feb 18 12:39 CET "test_RungeKuttaFehlberg45Integrator" time elapsed: 00:00:00 ---------------------------------------------------------- 124/137 Testing: test_RungeKuttaFehlberg56Integrator 124/137 Test: test_RungeKuttaFehlberg56Integrator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_RungeKuttaFehlberg56Integrator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators "test_RungeKuttaFehlberg56Integrator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 4 test cases... *** No errors detected Test time = 0.05 sec ---------------------------------------------------------- Test Passed. "test_RungeKuttaFehlberg56Integrator" end time: Feb 18 12:39 CET "test_RungeKuttaFehlberg56Integrator" time elapsed: 00:00:00 ---------------------------------------------------------- 125/137 Testing: test_RungeKuttaFehlberg78Integrator 125/137 Test: test_RungeKuttaFehlberg78Integrator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_RungeKuttaFehlberg78Integrator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators "test_RungeKuttaFehlberg78Integrator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.03 sec ---------------------------------------------------------- Test Passed. "test_RungeKuttaFehlberg78Integrator" end time: Feb 18 12:39 CET "test_RungeKuttaFehlberg78Integrator" time elapsed: 00:00:00 ---------------------------------------------------------- 126/137 Testing: test_RungeKutta87DormandPrinceIntegrator 126/137 Test: test_RungeKutta87DormandPrinceIntegrator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_RungeKutta87DormandPrinceIntegrator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators "test_RungeKutta87DormandPrinceIntegrator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_RungeKutta87DormandPrinceIntegrator" end time: Feb 18 12:39 CET "test_RungeKutta87DormandPrinceIntegrator" time elapsed: 00:00:00 ---------------------------------------------------------- 127/137 Testing: test_RootFinders 127/137 Test: test_RootFinders Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_RootFinders" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/RootFinders "test_RootFinders" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 19 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_RootFinders" end time: Feb 18 12:39 CET "test_RootFinders" time elapsed: 00:00:00 ---------------------------------------------------------- 128/137 Testing: test_SimpleLinearRegression 128/137 Test: test_SimpleLinearRegression Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_SimpleLinearRegression" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/Statistics "test_SimpleLinearRegression" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 3 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_SimpleLinearRegression" end time: Feb 18 12:39 CET "test_SimpleLinearRegression" time elapsed: 00:00:00 ---------------------------------------------------------- 129/137 Testing: test_BasicStatistics 129/137 Test: test_BasicStatistics Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_BasicStatistics" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/Statistics "test_BasicStatistics" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.01 sec ---------------------------------------------------------- Test Passed. "test_BasicStatistics" end time: Feb 18 12:39 CET "test_BasicStatistics" time elapsed: 00:00:00 ---------------------------------------------------------- 130/137 Testing: test_MultiVariateProbabilityDistributions 130/137 Test: test_MultiVariateProbabilityDistributions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_MultiVariateProbabilityDistributions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/Statistics "test_MultiVariateProbabilityDistributions" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.04 sec ---------------------------------------------------------- Test Passed. "test_MultiVariateProbabilityDistributions" end time: Feb 18 12:39 CET "test_MultiVariateProbabilityDistributions" time elapsed: 00:00:00 ---------------------------------------------------------- 131/137 Testing: test_BoostDistributions 131/137 Test: test_BoostDistributions Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_BoostDistributions" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/Statistics "test_BoostDistributions" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 1 test case... *** No errors detected Test time = 0.02 sec ---------------------------------------------------------- Test Passed. "test_BoostDistributions" end time: Feb 18 12:39 CET "test_BoostDistributions" time elapsed: 00:00:00 ---------------------------------------------------------- 132/137 Testing: test_KernelDensityDistribution 132/137 Test: test_KernelDensityDistribution Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_KernelDensityDistribution" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/Statistics "test_KernelDensityDistribution" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 7 test cases... *** No errors detected Test time = 4.04 sec ---------------------------------------------------------- Test Passed. "test_KernelDensityDistribution" end time: Feb 18 12:39 CET "test_KernelDensityDistribution" time elapsed: 00:00:04 ---------------------------------------------------------- 133/137 Testing: test_RandomSampling 133/137 Test: test_RandomSampling Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_RandomSampling" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/Statistics "test_RandomSampling" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 1.56 sec ---------------------------------------------------------- Test Passed. "test_RandomSampling" end time: Feb 18 12:39 CET "test_RandomSampling" time elapsed: 00:00:01 ---------------------------------------------------------- 134/137 Testing: test_TrapezoidalIntegrator 134/137 Test: test_TrapezoidalIntegrator Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_TrapezoidalIntegrator" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/Mathematics/NumericalQuadrature "test_TrapezoidalIntegrator" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 2 test cases... *** No errors detected Test time = 0.10 sec ---------------------------------------------------------- Test Passed. "test_TrapezoidalIntegrator" end time: Feb 18 12:39 CET "test_TrapezoidalIntegrator" time elapsed: 00:00:00 ---------------------------------------------------------- 135/137 Testing: test_SpiceInterface 135/137 Test: test_SpiceInterface Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_SpiceInterface" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/External/SpiceInterface "test_SpiceInterface" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 7 test cases... *** No errors detected Test time = 0.14 sec ---------------------------------------------------------- Test Passed. "test_SpiceInterface" end time: Feb 18 12:39 CET "test_SpiceInterface" time elapsed: 00:00:00 ---------------------------------------------------------- 136/137 Testing: test_EnvironmentSetup 136/137 Test: test_EnvironmentSetup Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_EnvironmentSetup" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/SimulationSetup "test_EnvironmentSetup" start time: Feb 18 12:39 CET Output: ---------------------------------------------------------- Running 9 test cases... *** No errors detected Test time = 3.82 sec ---------------------------------------------------------- Test Passed. "test_EnvironmentSetup" end time: Feb 18 12:40 CET "test_EnvironmentSetup" time elapsed: 00:00:03 ---------------------------------------------------------- 137/137 Testing: test_AccelerationModelSetup 137/137 Test: test_AccelerationModelSetup Command: "/Users/gigilaan/tudatBundle/tudat/bin/unit_tests/test_AccelerationModelSetup" Directory: /Users/gigilaan/build-tudatBundle-Desktop-Default/tudat/Tudat/SimulationSetup "test_AccelerationModelSetup" start time: Feb 18 12:40 CET Output: ---------------------------------------------------------- Running 5 test cases... Warning, overriding existing angle of attack function in AerodynamicAngleCalculator Warning, overriding existing angle of sideslip function in AerodynamicAngleCalculator Warning, overriding existing bank angle function in AerodynamicAngleCalculator Warning, overriding existing angle of attack function in AerodynamicAngleCalculator Warning, overriding existing angle of sideslip function in AerodynamicAngleCalculator Warning, overriding existing bank angle function in AerodynamicAngleCalculator Warning, overriding existing angle of attack function in AerodynamicAngleCalculator Warning, overriding existing angle of sideslip function in AerodynamicAngleCalculator Warning, overriding existing bank angle function in AerodynamicAngleCalculator Warning, overriding existing angle of attack function in AerodynamicAngleCalculator Warning, overriding existing angle of sideslip function in AerodynamicAngleCalculator Warning, overriding existing bank angle function in AerodynamicAngleCalculator *** No errors detected Test time = 0.37 sec ---------------------------------------------------------- Test Passed. "test_AccelerationModelSetup" end time: Feb 18 12:40 CET "test_AccelerationModelSetup" time elapsed: 00:00:00 ---------------------------------------------------------- End testing: Feb 18 12:40 CET