O_SESSAME::NumericPropagator Class Reference

#include <NumericPropagator.h>

Inheritance diagram for O_SESSAME::NumericPropagator:

[legend]List of all members.

Public Member Functions
	NumericPropagator ()
virtual	~NumericPropagator ()
virtual void	Propagate (const vector< ssfTime > &_propTime, const Vector &_orbitInitConditions, const Vector &_attInitConditions)
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
OrbitHistory	m_OrbitStateMeshPoints
AttitudeHistory	m_AttitudeStateMeshPoints

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Constructor & Destructor Documentation

O_SESSAME::NumericPropagator::NumericPropagator (   )

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

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

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

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Member Function Documentation

void O_SESSAME::NumericPropagator::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 in O_SESSAME::AttitudeNumericPropagator, and O_SESSAME::CombinedNumericPropagator. Definition at line 30 of file AttitudeNumericPropagator.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.

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.

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.

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

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 in O_SESSAME::CombinedNumericPropagator. Definition at line 40 of file Propagator.cpp.

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

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 in O_SESSAME::AttitudeNumericPropagator, and O_SESSAME::CombinedNumericPropagator. Definition at line 45 of file Propagator.cpp.

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Member Data Documentation

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

Pointer to the Orbit Representation being propagated Definition at line 117 of file Propagator.h.

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

Pointer to the Attitude Representation being propagated Definition at line 119 of file Propagator.h.

OrbitHistory O_SESSAME::Propagator::m_OrbitStateMeshPoints [protected, inherited]

Collection of calculated orbit state mesh points Reimplemented in O_SESSAME::AttitudeNumericPropagator, and O_SESSAME::CombinedNumericPropagator. Definition at line 122 of file Propagator.h.

AttitudeHistory O_SESSAME::Propagator::m_AttitudeStateMeshPoints [protected, inherited]

Collection of calculated attitude state mesh points Reimplemented in O_SESSAME::AttitudeNumericPropagator, and O_SESSAME::CombinedNumericPropagator. Definition at line 124 of file Propagator.h.

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