sgp4/Observer.cpp

93 lines
2.3 KiB
C++

#include "Observer.h"
#include "Globals.h"
/*
* in degrees!
*/
Observer::Observer(const double latitude, const double longitude, const double altitude) {
geo_.latitude = DegreesToRadians(latitude);
geo_.longitude = DegreesToRadians(longitude);
geo_.altitude = 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_.longitude);
double sin_lat = sin(geo_.latitude);
double cos_lat = cos(geo_.latitude);
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 += kPI;
if (az < 0.0)
az += 2.0 * kPI;
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;
}