Definition in file testAttitudeIntegration.cpp.
#include "Matrix.h"
#include "RungeKuttaIntegrator.h"
#include "LinearInterpolator.h"
#include "Plot.h"
#include "Attitude.h"
#include "AttitudeState.h"
#include <vector.h>
Go to the source code of this file.
Functions | |
Vector | NullFunctor (const ssfTime &_pSSFTime, const OrbitState &_pOrbitState, const AttitudeState &_pAttitudeState) |
Vector | AttituteDynamics (const ssfTime &_time, const Vector &_integratingState, Orbit *_pOrbit, Attitude *_pAttitude, const Matrix &_parameters, const Functor &_forceFunctorPtr) |
Dynamic and Kinematic attitude equations using quaternion and angular velocities. | |
int | main () |
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Definition at line 23 of file testAttitudeIntegration.cpp. |
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Dynamic and Kinematic attitude equations using quaternion and angular velocities.
Definition at line 56 of file testAttitudeIntegration.cpp. |
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Definition at line 90 of file testAttitudeIntegration.cpp. |