O_SESSAME::CombinedNumericPropagator Class Reference

#include <CombinedNumericPropagator.h>

Inheritance diagram for O_SESSAME::CombinedNumericPropagator:

[legend]Collaboration diagram for O_SESSAME::CombinedNumericPropagator:

[legend]List of all members.

Public Member Functions
	CombinedNumericPropagator ()
virtual	~CombinedNumericPropagator ()
virtual void	Propagate (const vector< ssfTime > &_propTime, const Vector &_orbitInitConditions, const Vector &_attInitConditions)
void	SetOrbitIntegrator (Integrator *_pOrbitIntegrator)
void	SetAttitudeIntegrator (Integrator *_pAttitudeIntegrator)
Integrator *	GetOrbitIntegrator () const
Integrator *	GetAttitudeIntegrator () const
virtual void	Propagate (const vector< ssfTime > &_propTime)
	Propagates the dynamics forward through time.
virtual void	SetAttitudeObject (Attitude *_pAttitudeObject)
	Sets the Attitude Representation object to be propagated.
virtual void	SetOrbitObject (Orbit *_pOrbitObject)
	Sets the Orbit Representation object to be propagated.
Protected Member Functions
virtual Matrix	PropagateOrbit (const vector< ssfTime > &_propTime, const Vector &_initConditions)
	Propagate the orbit through a specified time.
virtual Matrix	PropagateAttitude (const vector< ssfTime > &_propTime, const Vector &_initConditions)
	Propagate the attitude through a specified time.
Protected Attributes
Orbit *	m_pOrbitObject
Attitude *	m_pAttitudeObject
Private Attributes
Matrix	m_OrbitStateMeshPoints
	Matrix of calculated integration mesh points for the orbit dynamics.
Matrix	m_AttitudeStateMeshPoints
	Matrix of calculated integration mesh points for the attitude dynamics.
Integrator *	m_pOrbitIntegrator
	pointer to the integrator used by the numeric propagator for orbit integration.
Integrator *	m_pAttitudeIntegrator
	pointer to the integrator used by the numeric propagator for attitude integration.

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Constructor & Destructor Documentation

O_SESSAME::CombinedNumericPropagator::CombinedNumericPropagator (   )

Default Constructor Definition at line 16 of file CombinedNumericPropagator.cpp.

O_SESSAME::CombinedNumericPropagator::~CombinedNumericPropagator (   )  [virtual]

Default Deconstructor Definition at line 21 of file CombinedNumericPropagator.cpp.

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Member Function Documentation

Integrator * O_SESSAME::CombinedNumericPropagator::GetAttitudeIntegrator (   )  const

Definition at line 141 of file CombinedNumericPropagator.cpp.

Integrator * O_SESSAME::CombinedNumericPropagator::GetOrbitIntegrator (   )  const

Definition at line 137 of file CombinedNumericPropagator.cpp.

void O_SESSAME::Propagator::Propagate (  const vector< ssfTime > &  _propTime  )  [virtual, inherited]

Propagates the dynamics forward through time. Parameters: _propTime  STL vector of values specifying beginning, ending times of propagation as well as time step [initialTime, timeStep, finalTime] (s) Reimplemented in O_SESSAME::AnalyticPropagator. Definition at line 22 of file Propagator.cpp. Referenced by O_SESSAME::Attitude::Propagate().

void O_SESSAME::CombinedNumericPropagator::Propagate (  const vector< ssfTime > &  _propTime, const Vector &  _orbitInitConditions, const Vector &  _attInitConditions )  [virtual]

Propagates the dynamics forward through time Parameters: _propTime  vector of ssfTime values specifying beginning, ending times of propagation as well as time step [initialTime, timeStep, finalTime] (s) _orbitInitConditions  initial conditions of the orbit integration. _attInitConditions  initial conditions of the attitude integration. Reimplemented from O_SESSAME::NumericPropagator. Definition at line 30 of file CombinedNumericPropagator.cpp. References O_SESSAME::Attitude::IsIntegrateable(), O_SESSAME::Orbit::IsIntegrateable(), PropagateAttitude(), PropagateOrbit(), and O_SESSAME::Vector. Referenced by Propagate().

Matrix O_SESSAME::CombinedNumericPropagator::PropagateAttitude (  const vector< ssfTime > &  _propTime, const Vector &  _initConditions )  [protected, virtual]

Propagate the attitude through a specified time. Parameters: _propTime  Vector of values specifying beginning, ending times of propagation as well as time step [initialTime, timeStep, finalTime] (s) _initConditions  Vector of initial conditions of the attitude propagation. Returns: Matrix of integrated times and states as returned by the attitude dynamics equation Reimplemented from O_SESSAME::Propagator. Definition at line 88 of file CombinedNumericPropagator.cpp. References _, O_SESSAME::Attitude::GetDynamicsEq(), O_SESSAME::Orbit::GetStateObject(), O_SESSAME::Attitude::GetStateObject(), CAMdoubleMatrix::initialize(), O_SESSAME::Integrator::Integrate(), m_AttitudeStateMeshPoints, m_pAttitudeIntegrator, O_SESSAME::Matrix, O_SESSAME::MatrixColsIndex, O_SESSAME::MatrixIndexBase, and O_SESSAME::Vector. Referenced by Propagate().

Matrix O_SESSAME::CombinedNumericPropagator::PropagateOrbit (  const vector< ssfTime > &  _propTime, const Vector &  _initConditions )  [protected, virtual]

Propagate the orbit through a specified time. Parameters: _propTime  vector of values specifying beginning, ending times of propagation as well as time step [initialTime, timeStep, finalTime] (s) _initConditions  Vector of initial conditions of the orbit propagation. Returns: Matrix of integrated times and states as returned by the orbit dynamics equation Reimplemented from O_SESSAME::Propagator. Definition at line 48 of file CombinedNumericPropagator.cpp. References _, O_SESSAME::Orbit::GetDynamicsEq(), O_SESSAME::Orbit::GetStateObject(), CAMdoubleMatrix::initialize(), O_SESSAME::Integrator::Integrate(), m_OrbitStateMeshPoints, m_pOrbitIntegrator, O_SESSAME::Matrix, O_SESSAME::MatrixColsIndex, O_SESSAME::MatrixIndexBase, and O_SESSAME::Vector. Referenced by Propagate().

void O_SESSAME::CombinedNumericPropagator::SetAttitudeIntegrator (  Integrator *  _pAttitudeIntegrator  )

Definition at line 132 of file CombinedNumericPropagator.cpp. References m_pAttitudeIntegrator. Referenced by SetupPropagator().

void O_SESSAME::Propagator::SetAttitudeObject (  Attitude *  _pAttitudeObject  )  [virtual, inherited]

Sets the Attitude Representation object to be propagated. Parameters: _AttitudeObject  pointer to the attitude representation Definition at line 30 of file Propagator.cpp. References O_SESSAME::Propagator::m_pAttitudeObject. Referenced by O_SESSAME::Attitude::SetPropagator().

void O_SESSAME::CombinedNumericPropagator::SetOrbitIntegrator (  Integrator *  _pOrbitIntegrator  )

Definition at line 127 of file CombinedNumericPropagator.cpp. References m_pOrbitIntegrator. Referenced by SetupPropagator().

void O_SESSAME::Propagator::SetOrbitObject (  Orbit *  _pOrbitObject  )  [virtual, inherited]

Sets the Orbit Representation object to be propagated. Parameters: _OrbitObject  pointer to the Orbit representation Definition at line 35 of file Propagator.cpp. References O_SESSAME::Propagator::m_pOrbitObject. Referenced by O_SESSAME::Orbit::SetPropagator().

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Member Data Documentation

Matrix O_SESSAME::CombinedNumericPropagator::m_AttitudeStateMeshPoints [private]

Matrix of calculated integration mesh points for the attitude dynamics. Reimplemented from O_SESSAME::Propagator. Definition at line 70 of file CombinedNumericPropagator.h. Referenced by PropagateAttitude().

Matrix O_SESSAME::CombinedNumericPropagator::m_OrbitStateMeshPoints [private]

Matrix of calculated integration mesh points for the orbit dynamics. Reimplemented from O_SESSAME::Propagator. Definition at line 68 of file CombinedNumericPropagator.h. Referenced by PropagateOrbit().

Integrator* O_SESSAME::CombinedNumericPropagator::m_pAttitudeIntegrator [private]

pointer to the integrator used by the numeric propagator for attitude integration. Definition at line 75 of file CombinedNumericPropagator.h. Referenced by PropagateAttitude(), and SetAttitudeIntegrator().

Attitude* O_SESSAME::Propagator::m_pAttitudeObject [protected, inherited]

Pointer to the Attitude Representation being propagated Definition at line 119 of file Propagator.h. Referenced by O_SESSAME::Propagator::SetAttitudeObject().

Integrator* O_SESSAME::CombinedNumericPropagator::m_pOrbitIntegrator [private]

pointer to the integrator used by the numeric propagator for orbit integration. Definition at line 73 of file CombinedNumericPropagator.h. Referenced by PropagateOrbit(), and SetOrbitIntegrator().

Orbit* O_SESSAME::Propagator::m_pOrbitObject [protected, inherited]

Pointer to the Orbit Representation being propagated Definition at line 117 of file Propagator.h. Referenced by O_SESSAME::Propagator::SetOrbitObject().

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The documentation for this class was generated from the following files:

• CombinedNumericPropagator.h
• CombinedNumericPropagator.cpp

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