Uses of Class
fr.cnes.sirius.patrius.orbits.orbitalparameters.ReentryParameters

Packages that use ReentryParameters

Package	Description
fr.cnes.sirius.patrius.orbits.orbitalparameters

Uses of ReentryParameters in fr.cnes.sirius.patrius.orbits.orbitalparameters

Methods in fr.cnes.sirius.patrius.orbits.orbitalparameters that return ReentryParameters

Modifier and Type	Method and Description
ReentryParameters	KeplerianParameters.getReentryParameters(double ae, double f) Convert current orbital parameters into reentry parameters.
ReentryParameters	EquinoctialParameters.getReentryParameters(double ae, double f) Convert current orbital parameters into reentry parameters.
ReentryParameters	ApsisAltitudeParameters.getReentryParameters(double req, double f) Convert current orbital parameters into reentry parameters.
ReentryParameters	AlternateEquinoctialParameters.getReentryParameters(double ae, double f) Convert current orbital parameters into reentry parameters.
ReentryParameters	IOrbitalParameters.getReentryParameters(double ae, double f) Convert current orbital parameters into reentry parameters.
ReentryParameters	ReentryParameters.getReentryParameters(double req, double flat) Convert current orbital parameters into reentry parameters.
ReentryParameters	CartesianParameters.getReentryParameters(double ae, double f) Convert current orbital parameters into reentry parameters.
ReentryParameters	StelaEquinoctialParameters.getReentryParameters(double ae, double f) Convert current orbital parameters into reentry parameters.
ReentryParameters	EquatorialParameters.getReentryParameters(double ae, double f) Convert current orbital parameters into reentry parameters.
ReentryParameters	ApsisRadiusParameters.getReentryParameters(double ae, double f) Convert current orbital parameters into reentry parameters.
ReentryParameters	CircularParameters.getReentryParameters(double ae, double f) Convert current orbital parameters into reentry parameters.
ReentryParameters	CartesianParameters.getReentryParameters(double ae, double f, double mu) Convert current orbital parameters into reentry parameters.