Collaboration diagram for SatGeom:

Data Fields
SatSys	Sat
	Satellite.

VectorEcef	rSat
	Satellite position (ECEF)

VectorEcef	vSat
	Satellite velocity (ECEF)

VectorEcef	vSatPrime
	Satellite velocity (ECEF + Earth rotation component)

VectorEcef	rSun
	Sun position (ECEF)

VectorEcef	rMoon
	Moon position (ECEF)

VectorEcef	eNorm
	Normalised orbit normal vector (ECEF)

double	beta = 0
	Sun elevation angle with respect to the orbital plane.

double	betaRate = 0
	dBeta/dt

double	mu = 0
	Angle of sat from 'midnight' (when sat is at the furthest point from Sun in its orbit)

double	muRate = 0
	dMu/dt

Field Documentation

◆ beta

double SatGeom::beta = 0

Sun elevation angle with respect to the orbital plane.

◆ betaRate

double SatGeom::betaRate = 0

dBeta/dt

◆ eNorm

VectorEcef SatGeom::eNorm

Normalised orbit normal vector (ECEF)

◆ mu

double SatGeom::mu = 0

Angle of sat from 'midnight' (when sat is at the furthest point from Sun in its orbit)

◆ muRate

double SatGeom::muRate = 0

dMu/dt

◆ rMoon

VectorEcef SatGeom::rMoon

Moon position (ECEF)

◆ rSat

VectorEcef SatGeom::rSat

Satellite position (ECEF)

◆ rSun

VectorEcef SatGeom::rSun

Sun position (ECEF)

◆ Sat

SatSys SatGeom::Sat

Satellite.

◆ vSat

VectorEcef SatGeom::vSat

Satellite velocity (ECEF)

◆ vSatPrime

VectorEcef SatGeom::vSatPrime

Satellite velocity (ECEF + Earth rotation component)

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

/ginan/src/cpp/common/attitude.cpp

Data Fields