Element Access functions
[Orbit State Represenations]

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Detailed Description

Functions to access the specific elements of the Keplerian Orbital Elements.

Functions
double	GetSemiParameter () const
	Compute and return the Semiparameter of the orbit position.
double	GetSemimajorAxis () const
	Return the Semimajor Axis of the orbit position. (km).
double	GetEccentricity () const
	Return the Eccentricity of the orbit position. (-).
double	GetInclination () const
	Return the Inclination of the orbit position. (-).
double	GetLongAscNode () const
	Return the Longitude of the Ascending Node of the orbit position. (rad).
double	GetArgPerigee () const
	Return the Argument of Perigee of the orbit position. (rad).
double	GetTrueAnomaly () const
	Return the True Anomaly of the orbit position. (rad).
double	GetMeanMotion () const
	Return the Mean orbital motion of the orbit position. (rad/s).

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Function Documentation

double O_SESSAME::Keplerian::GetSemiParameter (   )  const [inherited]

Compute and return the Semiparameter of the orbit position. Returns: the semiparameter: . (km) Definition at line 119 of file Keplerian.h.

double O_SESSAME::Keplerian::GetSemimajorAxis (   )  const [inherited]

Return the Semimajor Axis of the orbit position. (km). Definition at line 122 of file Keplerian.h.

double O_SESSAME::Keplerian::GetEccentricity (   )  const [inherited]

Return the Eccentricity of the orbit position. (-). Definition at line 125 of file Keplerian.h.

double O_SESSAME::Keplerian::GetInclination (   )  const [inherited]

Return the Inclination of the orbit position. (-). Definition at line 128 of file Keplerian.h.

double O_SESSAME::Keplerian::GetLongAscNode (   )  const [inherited]

Return the Longitude of the Ascending Node of the orbit position. (rad). Definition at line 131 of file Keplerian.h.

double O_SESSAME::Keplerian::GetArgPerigee (   )  const [inherited]

Return the Argument of Perigee of the orbit position. (rad). Definition at line 134 of file Keplerian.h.

double O_SESSAME::Keplerian::GetTrueAnomaly (   )  const [inherited]

Return the True Anomaly of the orbit position. (rad). Definition at line 137 of file Keplerian.h.

double O_SESSAME::Keplerian::GetMeanMotion (   )  const [inherited]

Return the Mean orbital motion of the orbit position. (rad/s). Definition at line 140 of file Keplerian.h.

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