Gauss propagator #165
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Gauss propagator #165
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…sity Reneh107 add kernel density
CMake Update
Changes (unsigned int to int) to suppress compiler warnings on MinGW …
…ty: no Setup/Updater allowed in name
… correcting small compilation warnings.
…bility Changed name of several unit test executables for Windows compatibili…
Fixing bug in rotational ephemerides Tudat#147)
…ntegrator/propagator settings are NULL
Simplified saving of third-body accelerations; added checks whether i…
Changing unit test tolerances to in response to issue Tudat#145
…ral body. Propagation of 3 solar system bodies partlt passing. Earth begins propagation with 7 cm orbit difference between Cowell and Gauss (???).
…e not yet exploiting long double state
…ted implementation of Gauss-Modified Equinoctial scheme
…quations to make it work.... Should check what is going on
… errors throughout Tudat
…erformance of Keplerian<->Cartesian conversion
…rect conversion MEE<->Cartesian with flipped singularity
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This code contains functionality for the propagation of both Kepler and modified Equinoctial elements (MEE) using a Gauss formulation of the equations of motion.
For the MEE case, only the propagation with the singularity at 180 degrees inclination is implemented. A warning is given if the initial inclination of any of the propagated bodies is greater than 90 degrees.