orbits.hpp File Reference

Functions
VectorEci	keplers2Inertial (Trace &trace, const Vector6d &keplers0)
bool	inertial2Keplers (Trace &trace, const VectorEci &r, const VectorEci &v, Vector6d &keplers)
VectorEci	propagateEllipse (Trace &trace, GTime time, double dt, const VectorEci &rSat, const VectorEci &vSat, SatPos &satPos, bool j2=false)
VectorEci	propagateFull (Trace &trace, GTime time, double dt, VectorEci &rSat, VectorEci &vSat, SatPos &satPos)

Function Documentation

inertial2Keplers()

bool inertial2Keplers	(	Trace &	trace,
		const VectorEci &	r,
		const VectorEci &	v,
		Vector6d &	keplers )

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keplers2Inertial()

VectorEci keplers2Inertial	(	Trace &	trace,
		const Vector6d &	keplers0 )

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propagateEllipse()

VectorEci propagateEllipse	(	Trace &	trace,
		GTime	time,
		double	dt,
		const VectorEci &	rSat,
		const VectorEci &	vSat,
		SatPos &	satPos,
		bool	j2 = false )

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propagateFull()

VectorEci propagateFull	(	Trace &	trace,
		GTime	time,
		double	dt,
		VectorEci &	rSat,
		VectorEci &	vSat,
		SatPos &	satPos )

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