orbitProp.hpp File Reference

Data Structures
struct	EMP
struct	OrbitState
struct	OrbitIntegrator

Functions
OrbitState	operator* (const double lhs, const OrbitState &rhs)
Orbits	operator+ (const Orbits &lhs, const Orbits &rhs)
Orbits	operator* (const Orbits &lhs, const double rhs)
Orbits	operator* (const double rhs, const Orbits &lhs)
KFState	getOrbitFromState (Trace &trace, string id, const KFState &kfState)
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.
Orbits	prepareOrbits (Trace &trace, const KFState &kfState)
void	integrateOrbits (OrbitIntegrator &orbitPropagator, Orbits &orbits, double integrationPeriod, double dt)
void	addEmpStates (const EmpKalmans &satOpts, KFState &kfState, const string &id)
void	addNilDesignStates (const KalmanModel &model, KFState &kfState, const KF &kfType, int num, const string &id)
void	outputOrbitConfig (KFState &kfState, bool isSmoothed=false)

Typedefs
typedef vector< OrbitState >	Orbits

Typedef Documentation

Orbits

typedef vector<OrbitState> Orbits

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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getOrbitFromState()

KFState getOrbitFromState	(	Trace &	trace,
		string	id,
		const KFState &	kfState )

integrateOrbits()

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

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operator*() [1/3]

OrbitState operator* ( const double lhs, const OrbitState & rhs )

inline

operator*() [2/3]

Orbits operator* ( const double rhs, const Orbits & lhs )

inline

operator*() [3/3]

Orbits operator* ( const Orbits & lhs, const double rhs )

inline

operator+()

Orbits operator+ ( const Orbits & lhs, const Orbits & rhs )

inline

outputOrbitConfig()

void outputOrbitConfig	(	KFState &	kfState,
		bool	isSmoothed = false )

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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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