testInterface.cpp File Reference

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Detailed Description

Uses a text-based user interface to step through running a simulation.

Author:

Author

cakinli

Version:

Revision

1.1.1.1

Date:

Date

2005/04/26 17:41:00

Definition in file testInterface.cpp.

#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 "Disturbances/GravityFunctions.h"
#include "Disturbances/SimpleAerodynamicDisturbances.h"
#include "Plot.h"
#include <string>
#include <stdlib.h>
#include <sstream>

Include dependency graph for testInterface.cpp:

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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 ()
Vector	SimpleController (const ssfTime &_currentTime, const OrbitState &_currentOrbitState, const AttitudeState &_currentAttitudeState, const EnvFuncParamaterType &_parameterList)
void	myOrbitStateConvFunc (const Matrix &_meshPoint, OrbitState &_convertedOrbitState)
void	myAttitudeStateConvFunc (const Matrix &_meshPoint, AttitudeState &_convertedAttitudeState)
void	DisplayOrbit ()
void	DisplayAttitude ()
void	DisplayPropagator ()
int	DisplayMenu ()
void	Select ()
int	main ()
Vector	AttituteDynamics (const ssfTime &_time, const Vector &_integratingState, Orbit *_Orbit, Attitude *_Attitude, const Matrix &_parameters, const Functor &_forceFunctorPtr)
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

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

Definition at line 391 of file testInterface.cpp. References _, O_SESSAME::Functor::Call(), O_SESSAME::eye(), O_SESSAME::Attitude::GetStateObject(), O_SESSAME::Orbit::GetStateObject(), CAMmatrixBase::inverse(), O_SESSAME::Matrix, O_SESSAME::MatrixIndexBase, O_SESSAME::norm2(), O_SESSAME::skew(), O_SESSAME::Vector, and O_SESSAME::VectorIndexBase. Referenced by ChangeAttitude().

void ChangeAttitude (   )

Definition at line 416 of file testInterface.cpp. References AttituteDynamics(), DisplayAttitude(), O_SESSAME::eye(), O_SESSAME::Matrix, myAttitude, myAttitudeStateConvFunc(), O_SESSAME::AttitudeState::SetAngularVelocity(), O_SESSAME::Attitude::SetDynamicsEq(), O_SESSAME::Attitude::SetParameters(), O_SESSAME::AttitudeState::SetRotation(), O_SESSAME::Attitude::SetStateConversion(), O_SESSAME::Attitude::SetStateObject(), and O_SESSAME::Vector. Referenced by Select().

void ChangeAttitudeIntegrator (   )

void ChangeEnvironment (   )

Definition at line 241 of file testInterface.cpp. References O_SESSAME::Environment::AddForceFunction(), O_SESSAME::EnvFunction::AddParameter(), O_SESSAME::Environment::AddTorqueFunction(), GravityForceFunction(), myEnvironment, SimpleController(), and O_SESSAME::Vector. Referenced by Select().

void ChangeOrbit (   )

Definition at line 345 of file testInterface.cpp. References DisplayOrbit(), myOrbit, myOrbitStateConvFunc(), O_SESSAME::Orbit::SetDynamicsEq(), O_SESSAME::OrbitState::SetOrbitFrame(), O_SESSAME::OrbitState::SetState(), O_SESSAME::Orbit::SetStateConversion(), O_SESSAME::Orbit::SetStateObject(), O_SESSAME::OrbitState::SetStateRepresentation(), O_SESSAME::Vector, and O_SESSAME::VectorIndexBase. Referenced by Select().

void ChangeOrbitIntegrator (   )

void ChangePropagator (   )

Definition at line 299 of file testInterface.cpp. References attitudeIntegrator, DisplayPropagator(), orbitIntegrator, propTimes, O_SESSAME::RungeKuttaFehlbergIntegrator::SetStepSizes(), O_SESSAME::RungeKuttaFehlbergIntegrator::SetTolerance(), and stepSize. Referenced by Select().

void DisplayAttitude (   )

Definition at line 68 of file testInterface.cpp. References O_SESSAME::AttitudeState::GetState(), O_SESSAME::Attitude::GetStateObject(), O_SESSAME::Attitude::IsIntegrateable(), and myAttitude. Referenced by ChangeAttitude(), and DisplayMenu().

int DisplayMenu (   )

Definition at line 84 of file testInterface.cpp. References DisplayAttitude(), DisplayOrbit(), and DisplayPropagator(). Referenced by Select().

void DisplayOrbit (   )

Definition at line 59 of file testInterface.cpp. References O_SESSAME::OrbitStateRepresentation::GetPositionVelocity(), O_SESSAME::Orbit::GetStateObject(), O_SESSAME::OrbitState::GetStateRepresentation(), O_SESSAME::Orbit::IsIntegrateable(), and myOrbit. Referenced by ChangeOrbit(), and DisplayMenu().

void DisplayPropagator (   )

Definition at line 76 of file testInterface.cpp. References propTimes. Referenced by ChangePropagator(), and DisplayMenu().

int main (   )

Definition at line 146 of file testInterface.cpp. References O_SESSAME::AttitudeHistory::GetHistory(), O_SESSAME::OrbitHistory::GetHistory(), O_SESSAME::Attitude::GetHistoryObject(), O_SESSAME::Orbit::GetHistoryObject(), O_SESSAME::AttitudeHistory::GetState(), O_SESSAME::OrbitHistory::GetState(), O_SESSAME::Attitude::IsIntegrateable(), O_SESSAME::Orbit::IsIntegrateable(), myAttitude, myEnvironment, myOrbit, myPropagator, Select(), O_SESSAME::Attitude::SetEnvironment(), O_SESSAME::Orbit::SetEnvironment(), O_SESSAME::Attitude::SetPropagator(), O_SESSAME::Orbit::SetPropagator(), SetupAttitude(), SetupEnvironment(), SetupOrbit(), and SetupPropagator().

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

Definition at line 384 of file testInterface.cpp. References _, O_SESSAME::Matrix, O_SESSAME::AttitudeState::SetState(), and O_SESSAME::Vector. Referenced by ChangeAttitude().

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

Definition at line 337 of file testInterface.cpp. References _, O_SESSAME::Matrix, O_SESSAME::MatrixColsIndex, O_SESSAME::MatrixIndexBase, O_SESSAME::OrbitState::SetState(), and O_SESSAME::Vector. Referenced by ChangeOrbit().

void Plot (   )

Definition at line 188 of file testInterface.cpp. References _, O_SESSAME::AttitudeHistory::GetHistory(), O_SESSAME::OrbitHistory::GetHistory(), O_SESSAME::Attitude::GetHistoryObject(), O_SESSAME::Orbit::GetHistoryObject(), O_SESSAME::Attitude::IsIntegrateable(), O_SESSAME::Orbit::IsIntegrateable(), O_SESSAME::Matrix, O_SESSAME::MatrixIndexBase, myAttitude, myOrbit, O_SESSAME::Plot2D(), and O_SESSAME::Plot3D().

void Propagate (   )

Definition at line 207 of file testInterface.cpp. References O_SESSAME::AttitudeState::GetState(), O_SESSAME::OrbitState::GetState(), O_SESSAME::Attitude::GetStateObject(), O_SESSAME::Orbit::GetStateObject(), O_SESSAME::Attitude::IsIntegrateable(), O_SESSAME::Orbit::IsIntegrateable(), myAttitude, myOrbit, myPropagator, O_SESSAME::CombinedNumericPropagator::Propagate(), propTimes, O_SESSAME::ssfSeconds, O_SESSAME::tick(), and O_SESSAME::Vector. Referenced by Select().

void Select (   )

Definition at line 106 of file testInterface.cpp. References ChangeAttitude(), ChangeEnvironment(), ChangeOrbit(), ChangePropagator(), DisplayMenu(), and Propagate(). Referenced by main().

void SetupAttitude (   )

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

Environment * SetupEnvironment (   )

Definition at line 232 of file testInterface.cpp. References myEnvironment, and O_SESSAME::Environment::SetCentralBody(). Referenced by main().

void SetupOrbit (   )

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

void SetupPropagator (   )

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

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

Definition at line 454 of file testInterface.cpp. References O_SESSAME::ssfTime::GetSeconds(), and O_SESSAME::Vector. Referenced by ChangeEnvironment().

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Variable Documentation

RungeKuttaFehlbergIntegrator* attitudeIntegrator = NULL [static]

Definition at line 37 of file testInterface.cpp. Referenced by ChangePropagator().

Attitude* myAttitude = NULL [static]

Definition at line 33 of file testInterface.cpp. Referenced by ChangeAttitude(), DisplayAttitude(), main(), Plot(), and Propagate().

Environment* myEnvironment = NULL [static]

Definition at line 34 of file testInterface.cpp. Referenced by ChangeEnvironment(), main(), and SetupEnvironment().

Orbit* myOrbit = NULL [static]

Definition at line 32 of file testInterface.cpp. Referenced by ChangeOrbit(), DisplayOrbit(), main(), Plot(), and Propagate().

CombinedNumericPropagator* myPropagator = NULL [static]

Definition at line 35 of file testInterface.cpp. Referenced by main(), and Propagate().

RungeKuttaFehlbergIntegrator* orbitIntegrator = NULL [static]

Definition at line 36 of file testInterface.cpp. Referenced by ChangePropagator().

vector<ssfTime> propTimes [static]

Definition at line 38 of file testInterface.cpp. Referenced by ChangePropagator(), DisplayPropagator(), and Propagate().

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