Earth Observation Mission CFI Software Pointing Software User Manual for JAVA |
File Model for satellite attitude. More...
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< AttDataRec > | attData |
Array with the angle/quaternion records. | |
StarTrackerAux | auxData |
Auxiliary data. | |
Vector< StarTracker > | tmData |
tmData vector. |
File Model for satellite attitude.
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.
Array with the angle/quaternion records.
Auxiliary data.
Data type. Quaternions or angles (AttitudeDataTypeEnum).
Target reference frame.
Inertial frame.
double EECFI.SatAttFileModel.maxGap |
Maximum gap.
tmData vector.
Validity time 0.
Validity time 1.