testOrbitIntegration.cpp File Reference

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Detailed Description

Example of orbit integration using Open-Sessame.

Author:

Author

nilspace

Version:

Revision

1.3

Date:

Date

2003/05/13 18:56:15

Definition in file testOrbitIntegration.cpp.

#include "orbitmodels/TwoBodyDynamics.h"
#include "Matrix.h"
#include "RungeKuttaFehlbergIntegrator.h"
#include "OrbitState.h"
#include "Plot.h"
#include "orbitframes/OrbitFrameIJK.h"
#include "orbitstaterep/PositionVelocity.h"
#include "LinearInterpolator.h"
#include <vector.h>

Go to the source code of this file.

Functions
Vector	OrbitForcesFunctor (const ssfTime &_pSSFTime, const OrbitState &_pOrbitState, const AttitudeState &_pAttitudeState)
	Force function that will be called each timestep.
Vector	OrbitForcesWithDragFunctor (const ssfTime &_pSSFTime, const OrbitState &_pOrbitState, const AttitudeState &_pAttitudeState)
int	main ()

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Function Documentation

Vector OrbitForcesFunctor (  const ssfTime &  _pSSFTime, const OrbitState &  _pOrbitState, const AttitudeState &  _pAttitudeState )

Force function that will be called each timestep. Examples: testEnvironment.cpp, and testOrbitIntegration.cpp. Definition at line 26 of file testOrbitIntegration.cpp.

Vector OrbitForcesWithDragFunctor (  const ssfTime &  _pSSFTime, const OrbitState &  _pOrbitState, const AttitudeState &  _pAttitudeState )

Examples: testOrbitIntegration.cpp. Definition at line 34 of file testOrbitIntegration.cpp.

int main (   )

Definition at line 48 of file testOrbitIntegration.cpp.

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