Inheritance diagram for EECFI.AttitudeDef:

Public Member Functions
	AttitudeDef ()
	Empty Class constructor.
	AttitudeDef (long typeIn, SatNomTransId satNomTrIdIn, SatTransId satTrIdIn, InstrTransId instTrIdIn)
	Constructor with satellite frame ids. Only references are copied.
native void	attitudeTransform (final TransformCfg transformCfg) throws CfiError
	The reference frame in the attitude id can be changed using attitudeTransform.
Public Attributes
long	type
	XPCFI_SAT_NOMINAL_ATT/XPCFI_SAT_ATT/XPCFI_INSTR_ATT.
SatNomTransId	satNomTransId
	Satellite nominal attitude.
SatTransId	satTransId
	Satellite attitude.
InstrTransId	instrTransId
	Instrument attitude.

Detailed Description

Attitude definition data.

Constructor & Destructor Documentation

EECFI.AttitudeDef.AttitudeDef ( )

Empty Class constructor.

EECFI.AttitudeDef.AttitudeDef	(	long	typeIn,
		SatNomTransId	satNomTrIdIn,
		SatTransId	satTrIdIn,
		InstrTransId	instTrIdIn
	)

Constructor with satellite frame ids. Only references are copied.

Member Function Documentation

void EECFI.AttitudeDef::attitudeTransform ( final TransformCfg transformCfg ) throws CfiError

The reference frame in the attitude id can be changed using attitudeTransform.

Remark: all attitude related computations are performed in the True of Date Coordinate System. This means that, if one attitude id has been initialized with data expressed in another reference frame (e.g. attitude file with quaternions expressed in EF), at each call of a function using such attitude id (e.g. Attitude.compute) one or more conversions to True of Date will be performed. If the reference frame is changed to True of Date (using AttitudeDef.attitudeTransform), such conversions will not be executed and this will result in a run-time performance improvement.
Note: transformation of attitude ids that are initialized with Start Tracker files is not supported.

Parameters:

transformCfg

Transformation parameters.