Orbit Class Reference

#include <PME.h>

Public Member Functions
	Orbit ()
	~Orbit ()
void	calculate_eccentricity (CPoint R, CPoint V)
void	calculate_orbital_params (CPoint R, CPoint V)
void	calculate_absolute_position (CPoint &new_position)
void	calculate_new_position_in_orbit ()
void	dump ()

Protected Attributes
double	a
double	n
double	e
double	i
double	omega
double	w
double	nu
CPoint	e_vec
CPoint	n_vec
double	mu

Detailed Description

Definition at line 79 of file PME.h.

Constructor & Destructor Documentation

Orbit::Orbit ( )

inline

Definition at line 93 of file PME.h.

Orbit::~Orbit ( )

inline

Definition at line 94 of file PME.h.

Member Function Documentation

void Orbit::calculate_eccentricity	(	CPoint	R,
		CPoint	V
	)

Definition at line 204 of file PME.cpp.

References e, e_vec, error(), csl::CPoint::len(), mu, and csl::CPoint::normalize().

Referenced by calculate_orbital_params().

void Orbit::calculate_orbital_params	(	CPoint	R,
		CPoint	V
	)

Definition at line 182 of file PME.cpp.

References a, calculate_eccentricity(), e_vec, i, kTwoPi, csl::CPoint::len(), mu, n, n_vec, nu, omega, w, csl::CPoint::x, csl::CPoint::y, and csl::CPoint::z.

Referenced by PMESource::set_orbit().

void Orbit::calculate_absolute_position

(

CPoint &

new_position

)

Definition at line 257 of file PME.cpp.

References a, e, i, nu, omega, w, csl::CPoint::x, csl::CPoint::y, and csl::CPoint::z.

Referenced by PMESource::update_position().

void Orbit::calculate_new_position_in_orbit

(

)

Definition at line 265 of file PME.cpp.

References e, error(), kTwoPi, n, and nu.

Referenced by PMESource::update_position().

void Orbit::dump

(

void

)

Definition at line 288 of file PME.cpp.

References a, e, i, mu, nu, omega, and w.

Member Data Documentation

double Orbit::a

protected

Definition at line 81 of file PME.h.

Referenced by calculate_absolute_position(), calculate_orbital_params(), and dump().

double Orbit::n

protected

Definition at line 82 of file PME.h.

Referenced by calculate_new_position_in_orbit(), and calculate_orbital_params().

double Orbit::e

protected

Definition at line 83 of file PME.h.

Referenced by calculate_absolute_position(), calculate_eccentricity(), calculate_new_position_in_orbit(), and dump().

double Orbit::i

protected

Definition at line 84 of file PME.h.

Referenced by calculate_absolute_position(), calculate_orbital_params(), and dump().

double Orbit::omega

protected

Definition at line 85 of file PME.h.

Referenced by calculate_absolute_position(), calculate_orbital_params(), and dump().

double Orbit::w

protected

Definition at line 86 of file PME.h.

Referenced by calculate_absolute_position(), calculate_orbital_params(), and dump().

double Orbit::nu

protected

Definition at line 87 of file PME.h.

Referenced by calculate_absolute_position(), calculate_new_position_in_orbit(), calculate_orbital_params(), and dump().

CPoint Orbit::e_vec

protected

Definition at line 88 of file PME.h.

Referenced by calculate_eccentricity(), and calculate_orbital_params().

CPoint Orbit::n_vec

protected

Definition at line 89 of file PME.h.

Referenced by calculate_orbital_params().

double Orbit::mu

protected

Definition at line 90 of file PME.h.

Referenced by calculate_eccentricity(), calculate_orbital_params(), and dump().

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

• /Content/Code/CSL6/Src/Spatializers/VBAP/PME.h
• /Content/Code/CSL6/Src/Spatializers/VBAP/PME.cpp