/// Version without high-accuracy SolarSystem; cf. doc for other version.
double ComputeAtTransmitTime(const CommonTime& nomRecTime,
const double pr,
const Position& Rx,
const SatID sat,
const AntexData& antenna,
const XvtStore<SatID>& Eph)
throw(Exception)
{
// ssdummy will be invalid, so SolarPosition will be used;
// thus EarthOrientation will never be needed.
SolarSystem ssdummy;
EarthOrientation eodum;
return ComputeAtTransmitTime(nomRecTime,pr,Rx,sat,antenna,ssdummy,eodum,Eph);
}
/// Version with no antenna; cf. doc for other version.
double ComputeAtTransmitTime(const CommonTime& nomRecTime,
const double pr,
const Position& Rx,
const SatID sat,
const XvtStore<SatID>& Eph)
throw(Exception)
{
// antdummy will be invalid, so antenna computations will be skipped;
// thus SolarSystem and EarthOrientation will never be needed.
SolarSystem ssdum;
EarthOrientation eodum;
AntexData antdummy;
return ComputeAtTransmitTime(nomRecTime,pr,Rx,sat,antdummy,ssdum,eodum,Eph);
}
double CorrectedEphemerisRange::ComputeAtTransmitTime(
const CommonTime& tr_nom,
const Position& Rx,
const SatID sat,
const XvtStore<SatID>& Eph)
{
try {
gpstk::GPSEllipsoid gm;
svPosVel = Eph.getXvt(sat, tr_nom);
double pr = svPosVel.preciseRho(Rx, gm);
return ComputeAtTransmitTime(tr_nom, pr, Rx, sat, Eph);
}
catch(gpstk::Exception& e) {
GPSTK_RETHROW(e);
}
}
