Class DelaunayOE¶

Defined in File state.h

Inheritance Relationships¶

Base Type¶

public lupnt::State (Class State)

Class Documentation¶

class DelaunayOE : public lupnt::State ¶

Public Functions

inline DelaunayOE(const Vec6 &x = Vec6::Zero())¶

Construct a DelaunayOE (Delaunay orbital elements) from a stacked 6-element element vector. Used by element-set conversions in StateConverter for canonical Hamiltonian orbit representations.

Parameters:: x – [l, g, h, L, G, H], all in [rad].

inline DelaunayOE(const Vec6 &x, const Frame frame)¶

Construct a DelaunayOE from a stacked element vector and reference frame.

Parameters:

x – [l, g, h, L, G, H], all in [rad].
frame – Reference frame the elements are defined in.

inline Real &l()¶

Mutable reference to the mean longitude.

Returns:: Mean longitude [rad].

inline Real &g()¶

Mutable reference to the longitude of periapsis.

Returns:: Longitude of periapsis [rad].

inline Real &h()¶

Mutable reference to the longitude of ascending node.

Returns:: Longitude of ascending node [rad].

inline Real &L()¶

Mutable reference to the L Delaunay momentum.

Returns:: L [rad].

inline Real &G()¶

Mutable reference to the G Delaunay momentum.

Returns:: G [rad].

inline Real &H()¶

Mutable reference to the H Delaunay momentum.

Returns:: H [rad].

inline Real l() const¶

Mean longitude.

Returns:: Mean longitude [rad].

inline Real g() const¶

Longitude of periapsis.

Returns:: Longitude of periapsis [rad].

inline Real h() const¶

Longitude of ascending node.

Returns:: Longitude of ascending node [rad].

inline Real L() const¶

L Delaunay momentum.

Returns:: L [rad].

inline Real G() const¶

G Delaunay momentum.

Returns:: G [rad].

inline Real H() const¶

H Delaunay momentum.

Returns:: H [rad].

Public Static Attributes

static StateType TYPE = "DelaunayOE"¶