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When I print the aerodynamic moment coefficients and control surface deflection as dependent variables (in that order), in the actual output text file (computed by writeDataMapToTextFile) their column orders are reversed.
Thus the application output window says ;
Dependent variables being saved, output vectors contain:
Vector entry, Vector contents
0, Mach number of Aurora
1, Altitude of Aurora w.r.t. Earth
2, Aerodynamic moment coefficients of Aurora
3, Control Surface Deflectionof Aurora w.r.t. WingFlap
Whereas in the text file it actually is;
Dependent variables being saved, output vectors contain:
Vector entry, Vector contents
0, Mach number of Aurora
1, Altitude of Aurora w.r.t. Earth
2, Control Surface Deflectionof Aurora w.r.t. WingFlap
3, Aerodynamic moment coefficients of Aurora
The text was updated successfully, but these errors were encountered:
Thanks for opening this issue, I've uploaded a modification to the Github branch. For now, I would recommend not updating the branch directly, we're making a few modifications that may break your code if you do (nothing major, main change is that basic_mathematics::Vector6d will become Eigen::Vector6d). If you have a look at the changes of this commit:
you'll see that only propagationOutput.h is modified. Copy and paste these changes to this file on your machine, and the terminal output should match the file contents.
When I print the aerodynamic moment coefficients and control surface deflection as dependent variables (in that order), in the actual output text file (computed by writeDataMapToTextFile) their column orders are reversed.
Thus the application output window says ;
Dependent variables being saved, output vectors contain:
Vector entry, Vector contents
0, Mach number of Aurora
1, Altitude of Aurora w.r.t. Earth
2, Aerodynamic moment coefficients of Aurora
3, Control Surface Deflectionof Aurora w.r.t. WingFlap
Whereas in the text file it actually is;
Dependent variables being saved, output vectors contain:
Vector entry, Vector contents
0, Mach number of Aurora
1, Altitude of Aurora w.r.t. Earth
2, Control Surface Deflectionof Aurora w.r.t. WingFlap
3, Aerodynamic moment coefficients of Aurora
The text was updated successfully, but these errors were encountered: