testPropagation.cpp File Reference

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Detailed Description

Sample of an orbit and attitude propagation using components of the SSF.

Author:

Author

nilspace

Version:

Revision

1.4

Date:

Date

2003/05/27 17:47:13

Definition in file testPropagation.cpp.

#include "Matrix.h"
#include "Rotation.h"
#include "Attitude.h"
#include "Orbit.h"
#include "CombinedNumericPropagator.h"
#include "RungeKuttaIntegrator.h"
#include "orbitmodels/TwoBodyDynamics.h"
#include "EarthCentralBody.h"
#include "OrbitState.h"
#include "AttitudeState.h"
#include "orbitstaterep/PositionVelocity.h"
#include "orbitframes/OrbitFrameIJK.h"
#include "Plot.h"

Go to the source code of this file.

Functions
NumericPropagator *	SetupPropagator ()
	Sets up a combined numeric propagator, RK4(5) integrator and tolerances.
Environment *	SetupEnvironment ()
Orbit *	SetupOrbit ()
	Creates an initial orbit read in from a file.
Attitude *	SetupAttitude ()
	Creates an initial attitude read in from a file.
void	myOrbitStateConvFunc (const Matrix &_meshPoint, OrbitState &_convertedOrbitState)
void	myAttitudeStateConvFunc (const Matrix &_meshPoint, AttitudeState &_convertedAttitudeState)
int	main ()
Vector	GravityForceFunction (const ssfTime &_currentTime, const OrbitState &_currentOrbitState, const AttitudeState &_currentAttitudeState, const EnvFuncParamaterType &_parameterList)
Vector	DragForceFunction (const ssfTime &_currentTime, const OrbitState &_currentOrbitState, const AttitudeState &_currentAttitudeState, const EnvFuncParamaterType &_parameterList)
Vector	AttituteDynamics (const ssfTime &_time, const Vector &_integratingState, Orbit *_Orbit, Attitude *_Attitude, const Matrix &_parameters, const Functor &_forceFunctorPtr)

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Function Documentation

NumericPropagator* SetupPropagator (   )

Sets up a combined numeric propagator, RK4(5) integrator and tolerances. Definition at line 137 of file HokieSatSimulation.cpp.

Environment* SetupEnvironment (   )

Orbit* SetupOrbit (   )

Creates an initial orbit read in from a file. Definition at line 159 of file HokieSatSimulation.cpp.

Attitude* SetupAttitude (   )

Creates an initial attitude read in from a file. Definition at line 188 of file HokieSatSimulation.cpp.

void myOrbitStateConvFunc (  const Matrix &  _meshPoint, OrbitState &  _convertedOrbitState )

void myAttitudeStateConvFunc (  const Matrix &  _meshPoint, AttitudeState &  _convertedAttitudeState )

int main (   )

Definition at line 33 of file testPropagation.cpp.

Vector GravityForceFunction (  const ssfTime &  _currentTime, const OrbitState &  _currentOrbitState, const AttitudeState &  _currentAttitudeState, const EnvFuncParamaterType &  _parameterList )

Definition at line 108 of file testPropagation.cpp.

Vector DragForceFunction (  const ssfTime &  _currentTime, const OrbitState &  _currentOrbitState, const AttitudeState &  _currentAttitudeState, const EnvFuncParamaterType &  _parameterList )

Definition at line 118 of file testPropagation.cpp.

Vector AttituteDynamics (  const ssfTime &  _time, const Vector &  _integratingState, Orbit *  _Orbit, Attitude *  _Attitude, const Matrix &  _parameters, const Functor &  _forceFunctorPtr )  [static]

Definition at line 225 of file testPropagation.cpp.

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