posProp.cpp File Reference

Functions
void	propLinear (double dt, string &id, GTime time, Vector3d &r, Vector3d &v, Vector4d &q, const Vector3d &gyroScale, const Vector3d &acclScale, const Vector3d &gyroBias, const Vector3d &acclBias)
void	integrateInertials (InertialIntegrator &inertialPropagator, Inertials &inertials, double integrationPeriod, double dtRequested)
KFState	getInertialFromState (Trace &trace, string str, const KFState &kfState)
	Get the estimated elements for a single satellite's orbit.
Inertials	prepareInertials (Trace &trace, const KFState &kfState)
void	applyInertials (Trace &trace, Inertials &inertials, KFState &kfState, GTime time, double tgap)
	Apply the prediction using the filter's state transition.
void	predictInertials (Trace &trace, KFState &kfState, GTime time)
	Use models to predict orbital motion and prepare state transition equations to implement those predictions in the filter.

Function Documentation

applyInertials()

void applyInertials	(	Trace &	trace,
		Inertials &	inertials,
		KFState &	kfState,
		GTime	time,
		double	tgap )

Apply the prediction using the filter's state transition.

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getInertialFromState()

KFState getInertialFromState	(	Trace &	trace,
		string	str,
		const KFState &	kfState )

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

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integrateInertials()

void integrateInertials	(	InertialIntegrator &	inertialPropagator,
		Inertials &	inertials,
		double	integrationPeriod,
		double	dtRequested )

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predictInertials()

void predictInertials	(	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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prepareInertials()

Inertials prepareInertials	(	Trace &	trace,
		const KFState &	kfState )

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propLinear()

void propLinear	(	double	dt,
		string &	id,
		GTime	time,
		Vector3d &	r,
		Vector3d &	v,
		Vector4d &	q,
		const Vector3d &	gyroScale,
		const Vector3d &	acclScale,
		const Vector3d &	gyroBias,
		const Vector3d &	acclBias )

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