#include "Observer.h" #include "Globals.h" /* * in degrees! */ Observer::Observer(const double latitude, const double longitude, const double altitude) { geo_.SetLatitude(Globals::Deg2Rad(latitude)); geo_.SetLongitude(Globals::Deg2Rad(longitude)); geo_.SetAltitude(altitude); UpdateObserversEci(Julian()); } Observer::Observer(const CoordGeodetic &geo) : geo_(geo) { UpdateObserversEci(Julian()); } Observer::~Observer(void) { } void Observer::UpdateObserversEci(const Julian &date) { if (observers_eci_.GetDate() != date) { observers_eci_ = Eci(date, geo_); } } /* * calculate lookangle between the observer and the passed in Eci object */ CoordTopographic Observer::GetLookAngle(const Eci &eci) { /* * update the observers Eci to match the time of the Eci passed in */ UpdateObserversEci(eci.GetDate()); /* * calculate differences */ Vector range_rate = eci.GetVelocity().Subtract(observers_eci_.GetVelocity()); Vector range = eci.GetPosition().Subtract(observers_eci_.GetPosition()); range.SetW(range.GetMagnitude()); /* * Calculate Local Mean Sidereal Time for observers longitude */ double theta = eci.GetDate().ToLocalMeanSiderealTime(geo_.GetLongitude()); double sin_lat = sin(geo_.GetLatitude()); double cos_lat = cos(geo_.GetLatitude()); double sin_theta = sin(theta); double cos_theta = cos(theta); double top_s = sin_lat * cos_theta * range.GetX() + sin_lat * sin_theta * range.GetY() - cos_lat * range.GetZ(); double top_e = -sin_theta * range.GetX() + cos_theta * range.GetY(); double top_z = cos_lat * cos_theta * range.GetX() + cos_lat * sin_theta * range.GetY() + sin_lat * range.GetZ(); double az = atan(-top_e / top_s); if (top_s > 0.0) az += Globals::PI(); if (az < 0.0) az += 2.0 * Globals::PI(); double el = asin(top_z / range.GetW()); double rate = range.Dot(range_rate) / range.GetW(); /* * azimuth in radians * elevation in radians * range in km * range rate in km/s */ CoordTopographic topo(az, el, range.GetW(), rate); return topo; }