physics::orbit::elements< T > Struct Template Reference

Set of six Keplerian elements required to uniquely identify an orbit. More...

#include <elements.hpp>

Public Types
typedef T	scalar_type
	Scalar type. More...

Public Attributes
scalar_type	ec
	Eccentricity (e). More...
scalar_type	a
	Semimajor axis (a). More...
scalar_type	in
	Inclination (i), in radians. More...
scalar_type	om
	Right ascension of the ascending node (OMEGA), in radians. More...
scalar_type	w
	Argument of periapsis (omega), in radians. More...
scalar_type	ma
	Mean anomaly (M) at epoch, in radians. More...

Detailed Description

template<class T>
struct physics::orbit::elements< T >

Set of six Keplerian elements required to uniquely identify an orbit.

Template Parameters

T	Scalar type.

Definition at line 36 of file elements.hpp.

Member Typedef Documentation

scalar_type

template<class T >

typedef T physics::orbit::elements< T >::scalar_type

Scalar type.

Definition at line 39 of file elements.hpp.

Member Data Documentation

a

template<class T >

scalar_type physics::orbit::elements< T >::a

Semimajor axis (a).

Definition at line 45 of file elements.hpp.

ec

template<class T >

scalar_type physics::orbit::elements< T >::ec

Eccentricity (e).

Definition at line 42 of file elements.hpp.

in

template<class T >

scalar_type physics::orbit::elements< T >::in

Inclination (i), in radians.

Definition at line 48 of file elements.hpp.

ma

template<class T >

scalar_type physics::orbit::elements< T >::ma

Mean anomaly (M) at epoch, in radians.

Definition at line 57 of file elements.hpp.

om

template<class T >

scalar_type physics::orbit::elements< T >::om

Right ascension of the ascending node (OMEGA), in radians.

Definition at line 51 of file elements.hpp.

w

template<class T >

scalar_type physics::orbit::elements< T >::w

Argument of periapsis (omega), in radians.

Definition at line 54 of file elements.hpp.

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

• elements.hpp