Earth Observation Mission CFI Software Orbit Software User Manual for JAVA |
Outliers Data Filter Outliers Report. More...
Public Member Functions | |
OrbitDataFilterOutliersReport () | |
Empty constructor. | |
OrbitDataFilterOutliersReport (long in, long fi, double ming, double MaxG, double minp, double MaxP, double minv, double MaxV) | |
Constructor with parameters. | |
Public Attributes | |
long | nofOSVin |
Number of input orbit state vectors. | |
long | nofOSVfiltered |
Number of removed state vectors. | |
double | minTimeGap |
Minimum time gap between state vectors [seconds]. | |
double | maxTimeGap |
Maximum time gap between state vectors [seconds]. | |
double | minRMSPos |
Minimum RMS in position. | |
double | maxRMSPos |
Maximum RMS in position. | |
double | minRMSVel |
Minimum RMS in velocity. | |
double | maxRMSVel |
Maximum RMS in velocity. |
Outliers Data Filter Outliers Report.
EECFI.OrbitDataFilterOutliersReport.OrbitDataFilterOutliersReport | ( | ) |
Empty constructor.
EECFI.OrbitDataFilterOutliersReport.OrbitDataFilterOutliersReport | ( | long | in, | |
long | fi, | |||
double | ming, | |||
double | MaxG, | |||
double | minp, | |||
double | MaxP, | |||
double | minv, | |||
double | MaxV | |||
) |
Constructor with parameters.
Maximum RMS in position.
Maximum RMS in velocity.
Maximum time gap between state vectors [seconds].
Minimum RMS in position.
Minimum RMS in velocity.
Minimum time gap between state vectors [seconds].
Number of removed state vectors.
Number of input orbit state vectors.