orbitProp.cpp File Reference

Functions
Architecture	Orbit_Integrator__ ()
bool	queryVectorElement (vector< bool > &vec, size_t index)
void	integrateOrbits (OrbitIntegrator &orbitPropagator, Orbits &orbits, double integrationPeriod, double dtRequested)
shared_ptr< KFState >	getOrbitFromState (Trace &trace, SatSys Sat, string str, const KFState &kfState)
	Get the estimated elements for a single satellite's orbit.
Orbits	prepareOrbits (Trace &trace, const KFState &kfState)
void	applyOrbits (Trace &trace, Orbits &orbits, KFState &kfState, GTime time, double tgap)
	Apply the prediction using the filter's state transition.
void	predictOrbits (Trace &trace, KFState &kfState, GTime time)
	Use models to predict orbital motion and prepare state transition equations to implement those predictions in the filter.
void	addNilDesignStates (const KalmanModel &model, KFState &kfState, const KF &kfType, int num, const string &id)
void	addEmpStates (const EmpKalmans &satOpts, KFState &kfState, const string &id)
void	outputOrbitConfig (KFState &kfState, bool isSmoothed)

Function Documentation

addEmpStates()

void addEmpStates	(	const EmpKalmans &	satOpts,
		KFState &	kfState,
		const string &	id )

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addNilDesignStates()

void addNilDesignStates	(	const KalmanModel &	model,
		KFState &	kfState,
		const KF &	kfType,
		int	num,
		const string &	id )

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applyOrbits()

void applyOrbits	(	Trace &	trace,
		Orbits &	orbits,
		KFState &	kfState,
		GTime	time,
		double	tgap )

Apply the prediction using the filter's state transition.

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getOrbitFromState()

shared_ptr< KFState > getOrbitFromState	(	Trace &	trace,
		SatSys	Sat,
		string	str,
		const KFState &	kfState )

Get the estimated elements for a single satellite's orbit.

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integrateOrbits()

void integrateOrbits	(	OrbitIntegrator &	orbitPropagator,
		Orbits &	orbits,
		double	integrationPeriod,
		double	dtRequested )

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Orbit_Integrator__()

Architecture Orbit_Integrator__

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outputOrbitConfig()

void outputOrbitConfig	(	KFState &	kfState,
		bool	isSmoothed )

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predictOrbits()

void predictOrbits	(	Trace &	trace,
		KFState &	kfState,
		GTime	time )

Use models to predict orbital motion and prepare state transition equations to implement those predictions in the filter.

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prepareOrbits()

Orbits prepareOrbits	(	Trace &	trace,
		const KFState &	kfState )

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queryVectorElement()

bool queryVectorElement	(	vector< bool > &	vec,
		size_t	index )

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