Earth Observation Mission CFI Software Pointing Software User Manual for JAVA |
File Model for Nominal attitude and instrument attitude. More...
Public Member Functions | |
AttFileModel () | |
Empty constructor. | |
AttFileModel (long fileModel, double valTime0, double valTime1, long dataType, long inertialFrame, double maxGap, final Vector< AttDataRec > attDataIn) | |
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 |
Internal frame. | |
double | maxGap |
Maximum gap. | |
Vector< AttDataRec > | attData |
Array with the angle/quaternion records. |
File Model for Nominal attitude and instrument attitude.
EECFI.AttFileModel.AttFileModel | ( | ) |
Empty constructor.
EECFI.AttFileModel.AttFileModel | ( | long | fileModel, | |
double | valTime0, | |||
double | valTime1, | |||
long | dataType, | |||
long | inertialFrame, | |||
double | maxGap, | |||
final Vector< AttDataRec > | attDataIn | |||
) |
Constructor with parameters.
Vector<AttDataRec> EECFI.AttFileModel.attData |
Array with the angle/quaternion records.
Data type. Quaternions or angles (AttitudeDataTypeEnum).
Target reference frame.
Internal frame.
double EECFI.AttFileModel.maxGap |
Maximum gap.
double EECFI.AttFileModel.valTime0 |
Validity time 0.
double EECFI.AttFileModel.valTime1 |
Validity time 1.