public class OrbitCorrection extends Object
Constructor and Description |
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OrbitCorrection(double dRadial,
double dAlongTrack,
double dCrossTrack,
double dotRadial,
double dotAlongTrack,
double dotCrossTrack)
Constructor.
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Modifier and Type | Method and Description |
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double |
getDeltaOrbitAlongTrack()
Get the along-track orbit correction for broadcast ephemeris.
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double |
getDeltaOrbitCrossTrack()
Get the cross-track orbit correction for broadcast ephemeris.
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double |
getDeltaOrbitRadial()
Get the radial orbit correction for broadcast ephemeris.
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double |
getDotOrbitDeltaAlongTrack()
Get the velocity of along-track orbit correction for broadcast ephemeris.
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double |
getDotOrbitDeltaCrossTrack()
Get the velocity of cross-track orbit correction for broadcast ephemeris.
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double |
getDotOrbitDeltaRadial()
Get the velocity of radial orbit correction for broadcast ephemeris.
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public OrbitCorrection(double dRadial, double dAlongTrack, double dCrossTrack, double dotRadial, double dotAlongTrack, double dotCrossTrack)
dRadial
- radial orbit correction for broadcast ephemeris (m)dAlongTrack
- along-Track orbit correction for broadcast ephemeris (m)dCrossTrack
- cross-Track orbit correction for broadcast ephemeris (m)dotRadial
- velocity of Radial orbit correction for broadcast ephemeris. (m/s)dotAlongTrack
- velocity of Along-Track orbit correction for broadcast ephemeris (m/s)dotCrossTrack
- velocity of Cross-Track orbit correction for broadcast ephemeris (m/s)public double getDeltaOrbitRadial()
The reference time t0 is SSR Epoch Time (IDF003) plus ½ SSR Update Interval.
public double getDeltaOrbitAlongTrack()
The reference time t0 is SSR Epoch Time (IDF003) plus ½ SSR Update Interval.
public double getDeltaOrbitCrossTrack()
The reference time t0 is SSR Epoch Time (IDF003) plus ½ SSR Update Interval.
public double getDotOrbitDeltaRadial()
The reference time t0 is SSR Epoch Time (IDF003) plus ½ SSR Update Interval.
public double getDotOrbitDeltaAlongTrack()
The reference time t0 is SSR Epoch Time (IDF003) plus ½ SSR Update Interval.
public double getDotOrbitDeltaCrossTrack()
The reference time t0 is SSR Epoch Time (IDF003) plus ½ SSR Update Interval.
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