Go to the documentation of this file.
52 const double refLonRad)
54 compute( refLatRad, refLonRad );
75 const double refLonRad )
77 compute( refLatRad, refLonRad );
Matrix & resize(size_t rows, size_t cols)
Triple v
satellite velocity in ECEF Cartesian, meters/second
double sin(gnsstk::Angle x)
double relcorr
relativity correction (standard 2R.V/c^2 term), seconds
Triple x
Sat position ECEF Cartesian (X,Y,Z) meters.
double clkdrift
satellite clock drift in seconds/second
void updatePosition(const double refLatRad, const double refLonRad)
double cos(gnsstk::Angle x)
NEDUtil(const double refGdLatRad, const double refLonRad)
void compute(const double refLat, const double refLon)
gnsstk::Vector< double > convertToNED(const gnsstk::Vector< double > &inV) const
size_t size() const
STL size.
#define GNSSTK_THROW(exc)
double clkbias
Sat clock correction in seconds.
gnsstk
Author(s):
autogenerated on Wed Oct 25 2023 02:40:40