public Object clone()
{
SatellitePosition sp = new SatellitePosition(this.unixTime, this.satID, this.satType, this.getX(), this.getY(), this.getZ());
sp.maneuver = this.maneuver;
sp.predicted = this.predicted;
sp.satelliteClockError = this.satelliteClockError;
sp.setSpeed(speed.get(0), speed.get(1), speed.get(2));
return(sp);
}
public void setSatelliteVelocity(SatellitePosition satelliteVelocity)
{
this.satelliteVelocity = satelliteVelocity;
}
/**
* Calculates current correction for given parameters
* @param currentTime current timestamp
* @param approximatedPose approximate pose of the receiver
* @param satelliteCoordinates satellite coordinates
* @param navigationProducer Klobuchar coefficients from the naivgation message (ephemeris)
* @return calculated correction to be applied to the pseudorange
*/
public abstract void calculateCorrection(
Time currentTime,
Coordinates <Matrix> approximatedPose,
SatellitePosition satelliteCoordinates,
NavigationProducer navigationProducer,
Location initialLocation);
public void setSatellitePosition(SatellitePosition satellitePosition)
{
this.satellitePosition = satellitePosition;
this.clockBias = satellitePosition.getSatelliteClockError() * Constants.SPEED_OF_LIGHT; //todo: add this as a separate correction.
}