testEnvironment.cpp File Reference

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Detailed Description

Sample of an orbit integration and an Environment object using components of the SSF.

Author:

Author

cakinli

Version:

Revision

1.1.1.1

Date:

Date

2005/04/26 17:41:00

Definition in file testEnvironment.cpp.

#include "orbitmodels/TwoBodyDynamics.h"
#include "Matrix.h"
#include "RungeKuttaIntegrator.h"
#include "PositionVelocity.h"
#include "Plot.h"
#include "Environment.h"
#include "OrbitStateRepresentation.h"
#include "EarthCentralBody.h"
#include "OrbitState.h"
#include "orbitframes/OrbitFrameIJK.h"

Include dependency graph for testEnvironment.cpp:

Go to the source code of this file.

Functions
Vector	GravityForceFunction (ssfTime *_currentTime, OrbitState *_currentOrbitState, AttitudeState *_currentAttitudeState, EnvFuncParamaterType _parameterList)
Vector	DragForceFunction (ssfTime *_currentTime, OrbitState *_currentOrbitState, AttitudeState *_currentAttitudeState, EnvFuncParamaterType _parameterList)
int	main ()

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Function Documentation

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

Examples: testEnvironment.cpp. Definition at line 32 of file testEnvironment.cpp. References _, O_SESSAME::OrbitState::GetState(), O_SESSAME::norm2(), O_SESSAME::Vector, and O_SESSAME::VectorIndexBase. Referenced by main().

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

Definition at line 23 of file testEnvironment.cpp. References _, O_SESSAME::OrbitState::GetState(), O_SESSAME::norm2(), O_SESSAME::Vector, and O_SESSAME::VectorIndexBase.

int main (   )

Definition at line 42 of file testEnvironment.cpp. References _, O_SESSAME::Environment::AddForceFunction(), O_SESSAME::EnvFunction::AddParameter(), DragForceFunction(), O_SESSAME::ssfTime::GetSeconds(), O_SESSAME::OrbitState::GetState(), GravityForceFunction(), O_SESSAME::RungeKuttaIntegrator::Integrate(), O_SESSAME::Matrix, O_SESSAME::MatrixIndexBase, OrbitForcesFunctor(), O_SESSAME::Plot3D(), O_SESSAME::Environment::SetCentralBody(), O_SESSAME::RungeKuttaIntegrator::SetNumSteps(), O_SESSAME::OrbitState::SetOrbitFrame(), O_SESSAME::AttitudeState::SetRotation(), O_SESSAME::OrbitState::SetState(), O_SESSAME::OrbitState::SetStateRepresentation(), O_SESSAME::tick(), O_SESSAME::Vector, and O_SESSAME::VectorIndexBase.

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