Structure container for the Moon Keplerian orbital elements for orbit about the Earth. More...

#include <Planets.hh>

Public Member Functions
	KeplerianMoon ()
Public Member Functions inherited from Astro::OrbitalElements::Keplerian
	Keplerian ()
	Keplerian (Real const t_a, Real const t_e, Real const t_i, Real const t_Omega, Real const t_omega)
	Keplerian (Vector5 const &t_kepl)
	Keplerian (Keplerian const &)=default
	Keplerian (Keplerian &&)=default
Keplerian &	operator= (const Keplerian &)=default
Keplerian &	operator= (Keplerian &&)=default
Vector5	vector () const
std::string	info () const
void	info (std::ostream &os)
void	reset ()
bool	sanity_check () const
bool	is_singular (Real tol_i=EPSILON_LOW, Real tol_e=EPSILON_LOW) const
bool	is_nonsingular (Real tol_i=EPSILON_LOW, Real tol_e=EPSILON_LOW) const
Real	u () const
Real	p () const

Additional Inherited Members
Public Attributes inherited from Astro::OrbitalElements::Keplerian
Real	a {QUIET_NAN}
Real	e {QUIET_NAN}
Real	i {QUIET_NAN}
Real	Omega {QUIET_NAN}
Real	omega {QUIET_NAN}

Detailed Description

Structure container for the Moon Keplerian orbital elements for orbit about the Earth, which are:

the semi-major axis \( a = 0.002569555 \) (AU),
the eccentricity \( e = 0.0549006 \) (-),
the inclination \( i = 5.145396 \) (deg),
the longitude of the ascending node \( \Omega = 125.1228 \) (deg),
the argument of periapsis \( \omega = 318.0634 \) (deg).

Constructor & Destructor Documentation

Astro::Planets::KeplerianMoon::KeplerianMoon ( )

inline

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