Classical Keplerian orbital elements. More...

#include <perturb.hpp>

Public Member Functions
	ClassicalOrbitalElements (StateVector sv, GravModel grav_model=GravModel::WGS72)
	Construct from a `StateVector` position and velocity in TEME. More...

Public Attributes
double	semilatus_rectum
	Samilatus rectum in [km].

double	semimajor_axis
	Semimajor axis in [km].

double	eccentricity
	Eccentricity (unitless)

double	inclination
	Inlination in [rad].

double	raan
	Right ascension of ascending node in [rad].

double	arg_of_perigee
	Argument of perigee in [rad].

double	true_anomaly
	True anomaly in [rad].

double	mean_anomaly
	Mean anomaly in [rad].

double	arg_of_latitude
	Argument of latitude in [rad].

double	true_longitude
	True longitude in [rad].

double	longitude_of_periapsis
	Longitude of periapsis in [rad].

Detailed Description

Classical Keplerian orbital elements.

Names and values are from the underlying SGP4 implementation. Can be generated from a StateVector via the constructor.

Constructor & Destructor Documentation

perturb::ClassicalOrbitalElements::ClassicalOrbitalElements	(	StateVector	sv,
		GravModel	grav_model = `GravModel::WGS72`
	)

explicit

Construct from a StateVector position and velocity in TEME.

Parameters

sv	A position-velocity state vector generated via SGP4
grav_model	Gravity model used in SGP4 (default `GravModel::WGS72`)

The documentation for this struct was generated from the following files: