MemoryTest.cpp File Reference

#include "Matrix.h"
#include "Rotation.h"
#include "Attitude.h"
#include "Orbit.h"
#include "CombinedNumericPropagator.h"
#include "RungeKuttaFehlbergIntegrator.h"
#include "orbitmodels/TwoBodyDynamics.h"
#include "CentralBody/EarthCentralBody.h"
#include "OrbitState.h"
#include "AttitudeState.h"
#include "orbitstaterep/PositionVelocity.h"
#include "orbitframes/OrbitFrameIJK.h"
#include "Plot.h"
#include <string>
#include <stdlib.h>
#include <sstream>

Go to the source code of this file.

Functions
void	SetupPropagator ()
	Sets up a combined numeric propagator, RK4(5) integrator and tolerances.
void	SetupEnvironment ()
void	SetupOrbit ()
	Creates an initial orbit read in from a file.
void	SetupAttitude ()
	Creates an initial attitude read in from a file.
void	ChangePropagator ()
void	ChangeEnvironment ()
void	ChangeOrbit ()
void	ChangeOrbitIntegrator ()
void	ChangeAttitude ()
void	ChangeAttitudeIntegrator ()
void	Propagate ()
void	Plot ()
void	myOrbitStateConvFunc (const Matrix &_meshPoint, OrbitState &_convertedOrbitState)
void	myAttitudeStateConvFunc (const Matrix &_meshPoint, AttitudeState &_convertedAttitudeState)
void	DisplayOrbit ()
void	DisplayAttitude ()
void	DisplayPropagator ()
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)
	Dynamic and Kinematic attitude equations using quaternion and angular velocities.
Variables
Orbit *	myOrbit = NULL
Attitude *	myAttitude = NULL
Environment *	myEnvironment = NULL
CombinedNumericPropagator *	myPropagator = NULL
RungeKuttaFehlbergIntegrator *	orbitIntegrator = NULL
RungeKuttaFehlbergIntegrator *	attitudeIntegrator = NULL
vector< ssfTime >	propTimes

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Function Documentation

void SetupPropagator (   )

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

Environment * SetupEnvironment (   )

Definition at line 186 of file MemoryTest.cpp.

void SetupOrbit (   )

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

void SetupAttitude (   )

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

void ChangePropagator (   )

Definition at line 227 of file MemoryTest.cpp.

void ChangeEnvironment (   )

Definition at line 195 of file MemoryTest.cpp.

void ChangeOrbit (   )

Definition at line 260 of file MemoryTest.cpp.

void ChangeOrbitIntegrator (   )

void ChangeAttitude (   )

Definition at line 331 of file MemoryTest.cpp.

void ChangeAttitudeIntegrator (   )

void Propagate (   )

Definition at line 139 of file MemoryTest.cpp.

void Plot (   )

Definition at line 120 of file MemoryTest.cpp.

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

Examples: testPropagation.cpp. Definition at line 252 of file MemoryTest.cpp.

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

Examples: testPropagation.cpp. Definition at line 297 of file MemoryTest.cpp.

void DisplayOrbit (   )

Definition at line 56 of file MemoryTest.cpp.

void DisplayAttitude (   )

Definition at line 65 of file MemoryTest.cpp.

void DisplayPropagator (   )

Definition at line 73 of file MemoryTest.cpp.

int main (   )

Definition at line 82 of file MemoryTest.cpp.

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

Examples: testEnvironment.cpp, and testPropagation.cpp. Definition at line 175 of file MemoryTest.cpp.

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

Dynamic and Kinematic attitude equations using quaternion and angular velocities. Definition at line 304 of file MemoryTest.cpp.

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Variable Documentation

Orbit* myOrbit = NULL [static]

Definition at line 30 of file MemoryTest.cpp.

Attitude* myAttitude = NULL [static]

Definition at line 31 of file MemoryTest.cpp.

Environment* myEnvironment = NULL [static]

Definition at line 32 of file MemoryTest.cpp.

CombinedNumericPropagator* myPropagator = NULL [static]

Definition at line 33 of file MemoryTest.cpp.

RungeKuttaFehlbergIntegrator* orbitIntegrator = NULL [static]

Definition at line 34 of file MemoryTest.cpp.

RungeKuttaFehlbergIntegrator* attitudeIntegrator = NULL [static]

Definition at line 35 of file MemoryTest.cpp.

vector<ssfTime> propTimes [static]

Definition at line 36 of file MemoryTest.cpp.

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