DEIMOS
Earth Observation Mission CFI Software
Pointing Software User Manual
for JAVA
ESA

EECFI.SatAttFileModel Class Reference

File Model for satellite attitude. More...

List of all members.

Public Member Functions

 SatAttFileModel ()
 Empty constructor.
 SatAttFileModel (long fileModel, double valTime0, double valTime1, long dataType, long inertialFrame, double maxGap, final Vector< AttDataRec > attDataIn, final StarTrackerAux auxDat, final Vector< StarTracker > tmDat)
 Constructor with parameters.

Public Attributes

long fileModel
 Target reference frame.
double valTime0
 Validity time 0.
double valTime1
 Validity time 1.
long dataType
 Data type. Quaternions or angles (AttitudeDataTypeEnum).
long inertialFrame
 Inertial frame.
double maxGap
 Maximum gap.
Vector< AttDataRecattData
 Array with the angle/quaternion records.
StarTrackerAux auxData
 Auxiliary data.
Vector< StarTrackertmData
 tmData vector.

Detailed Description

File Model for satellite attitude.


Constructor & Destructor Documentation

EECFI.SatAttFileModel.SatAttFileModel (  ) 

Empty constructor.

EECFI.SatAttFileModel.SatAttFileModel ( long  fileModel,
double  valTime0,
double  valTime1,
long  dataType,
long  inertialFrame,
double  maxGap,
final Vector< AttDataRec attDataIn,
final StarTrackerAux  auxDat,
final Vector< StarTracker tmDat 
)

Constructor with parameters.


Member Data Documentation

Array with the angle/quaternion records.

Data type. Quaternions or angles (AttitudeDataTypeEnum).

Target reference frame.

Maximum gap.

tmData vector.

Validity time 0.

Validity time 1.


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