| Package | Description |
|---|---|
| agi.foundation.navigation.datareaders |
Contains types for reading various navigation-related data file formats.
|
| Modifier and Type | Method and Description |
|---|---|
SP3dEphemerisData<Double> |
SP3dEphemeris.getClockCorrection()
Gets the clock data, by Satellite Identifier.
|
SP3dEphemerisData<Double> |
SP3dEphemeris.getClockCorrectionRate()
Gets the clock correction rate data, by Satellite Identifier.
|
SP3dEphemerisData<Double> |
SP3dEphemeris.getClockCorrectionRateStandardDeviation()
Gets the standard deviations for the clock correction rate data, defined on the "EV" lines of
the SP3d file, by Satellite Identifier.
|
SP3dEphemerisData<Double> |
SP3dEphemeris.getClockCorrectionRateStandardDeviationApproximate()
Gets the approximate standard deviations for the clock correction data, defined on the same line as the
position data, by Satellite Identifier.
|
SP3dEphemerisData<Double> |
SP3dEphemeris.getClockCorrectionStandardDeviation()
Gets the standard deviations for the clock correction data, defined on the "EP" lines of the SP3d file,
by Satellite Identifier.
|
SP3dEphemerisData<Double> |
SP3dEphemeris.getClockCorrectionStandardDeviationApproximate()
Gets the approximate standard deviations for the clock correction data, defined on the same line as the
position data, by Satellite Identifier.
|
SP3dEphemerisData<JulianDate> |
SP3dEphemeris.getClockEvent()
Gets the clock event times as indicated by the clock event flag in the position 'P' record
If the flag is set for this time, there was a clock event after the previous epoch or at this epoch.
|
SP3dEphemerisData<JulianDate> |
SP3dEphemeris.getClockPredicted()
Gets the clock correction prediction times as indicated by the clock prediction flag in the position 'P' record
If the flag is set for this time, the clock correction for this time is predicted, otherwise it is not.
|
SP3dEphemerisData<JulianDate> |
SP3dEphemeris.getOrbitManeuver()
Gets the orbit maneuver times as indicated by the orbit maneuver flag in the position 'P' record
If the flag is set for this time, there was an orbit maneuver after the previous epoch or at this epoch.
|
SP3dEphemerisData<JulianDate> |
SP3dEphemeris.getOrbitPredicted()
Gets the orbit prediction times as indicated by the orbit prediction flag in the position 'P' record
If the flag is set for this time, the orbit for this time is predicted, otherwise it is not.
|
SP3dEphemerisData<SP3dCorrelations> |
SP3dEphemeris.getPositionCorrelations()
Gets the correlations for the position data, defined on the "EP" lines of the SP3d file,
by Satellite Identifier.
|
SP3dEphemerisData<Cartesian> |
SP3dEphemeris.getPositions()
Gets the position data, by Satellite Identifier.
|
SP3dEphemerisData<Cartesian> |
SP3dEphemeris.getPositionStandardDeviations()
Gets the standard deviations for the position data, defined on the "EP" lines of the SP3d file,
by Satellite Identifier.
|
SP3dEphemerisData<Cartesian> |
SP3dEphemeris.getPositionStandardDeviationsApproximate()
Gets the approximate standard deviations for the position data, defined on the same line as the
position data, by Satellite Identifier.
|
SP3dEphemerisData<Cartesian> |
SP3dEphemeris.getVelocities()
Gets the Velocity data, by Satellite Identifier.
|
SP3dEphemerisData<SP3dCorrelations> |
SP3dEphemeris.getVelocityCorrelations()
Gets the correlations for the velocity data, defined on the "EV" lines of the SP3d file,
by Satellite Identifier.
|
SP3dEphemerisData<Cartesian> |
SP3dEphemeris.getVelocityStandardDeviations()
Gets the standard deviations for the velocity data, defined on the "EV" lines of the SP3d file,
by Satellite Identifier.
|
SP3dEphemerisData<Cartesian> |
SP3dEphemeris.getVelocityStandardDeviationsApproximate()
Gets the approximate standard deviations for the velocity data, defined on the same line as the
velocity data, by Satellite Identifier.
|