Persistent data for yaw model. More...

Detailed Description

Persistent data for yaw model.

Collaboration diagram for AttStatus:

Data Fields
GTime	startTime
	Time of switchover to modified yaw steering (due to noon/midnight turn)

double	startSign = 0
	Sign of yaw rate at switchover.

double	startYaw = 0
	Yaw at switchover.

double	startYawRate = 0
	Yaw rate at switchover.

GTime	excludeTime
	Time to skip yaw modelling until, due to unknown yaw behaviour.

double	nominalYaw = 0
	Latest nominal yaw.

double	modelYaw = 0
	Latest modelled yaw (i.e. considering noon/midnight turns)

GTime	modelYawTime = GTime::noTime()
	Time of modelYaw (and nominalYaw)

bool	modelYawValid = false
	Model yaw was calculated sucessfully.

VectorEcef	eXBody
	X+ unit vector of body-fixed coordinates (ECEF)

VectorEcef	eYBody
	Y+ unit vector of body-fixed coordinates (ECEF)

VectorEcef	eZBody
	Z+ unit vector of body-fixed coordinates (ECEF)

VectorEcef	eXAnt
	X+ unit vector of antenna-fixed coordinates (ECEF)

VectorEcef	eYAnt
	Y+ unit vector of antenna-fixed coordinates (ECEF)

VectorEcef	eZAnt
	Z+ unit vector of antenna-fixed coordinates (ECEF)

Field Documentation

◆ eXAnt

VectorEcef AttStatus::eXAnt

X+ unit vector of antenna-fixed coordinates (ECEF)

◆ eXBody

VectorEcef AttStatus::eXBody

X+ unit vector of body-fixed coordinates (ECEF)

◆ excludeTime

GTime AttStatus::excludeTime

Initial value:

=

GTime::noTime()

GTime::noTime

static GTime noTime()

Uninitialised time for comparisons.

Definition gTime.hpp:145

Time to skip yaw modelling until, due to unknown yaw behaviour.

◆ eYAnt

VectorEcef AttStatus::eYAnt

Y+ unit vector of antenna-fixed coordinates (ECEF)

◆ eYBody

VectorEcef AttStatus::eYBody

Y+ unit vector of body-fixed coordinates (ECEF)

◆ eZAnt

VectorEcef AttStatus::eZAnt

Z+ unit vector of antenna-fixed coordinates (ECEF)

◆ eZBody

VectorEcef AttStatus::eZBody

Z+ unit vector of body-fixed coordinates (ECEF)

◆ modelYaw

double AttStatus::modelYaw = 0

Latest modelled yaw (i.e. considering noon/midnight turns)

◆ modelYawTime

GTime AttStatus::modelYawTime = GTime::noTime()

Time of modelYaw (and nominalYaw)

◆ modelYawValid

bool AttStatus::modelYawValid = false

Model yaw was calculated sucessfully.

◆ nominalYaw

double AttStatus::nominalYaw = 0

Latest nominal yaw.

◆ startSign

double AttStatus::startSign = 0

Sign of yaw rate at switchover.

◆ startTime

GTime AttStatus::startTime

Initial value:

= GTime::noTime(

)

Time of switchover to modified yaw steering (due to noon/midnight turn)

◆ startYaw

double AttStatus::startYaw = 0

Yaw at switchover.

◆ startYawRate

double AttStatus::startYawRate = 0

Yaw rate at switchover.

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

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