/* * Copyright 2013 Daniel Warner * * Licensed under the Apache License, Version 2.0 (the "License"); * you may not use this file except in compliance with the License. * You may obtain a copy of the License at * * http://www.apache.org/licenses/LICENSE-2.0 * * Unless required by applicable law or agreed to in writing, software * distributed under the License is distributed on an "AS IS" BASIS, * WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied. * See the License for the specific language governing permissions and * limitations under the License. */ #include "Observer.h" #include "CoordTopocentric.h" namespace libsgp4 { /* * calculate lookangle between the observer and the passed in Eci object */ CoordTopocentric Observer::GetLookAngle(const Eci &eci) { /* * update the observers Eci to match the time of the Eci passed in * if necessary */ Update(eci.GetDateTime()); /* * calculate differences */ Vector range_rate = eci.Velocity() - m_eci.Velocity(); Vector range = eci.Position() - m_eci.Position(); range.w = range.Magnitude(); /* * Calculate Local Mean Sidereal Time for observers longitude */ double theta = eci.GetDateTime().ToLocalMeanSiderealTime(m_geo.longitude); double sin_lat = sin(m_geo.latitude); double cos_lat = cos(m_geo.latitude); double sin_theta = sin(theta); double cos_theta = cos(theta); double top_s = sin_lat * cos_theta * range.x + sin_lat * sin_theta * range.y - cos_lat * range.z; double top_e = -sin_theta * range.x + cos_theta * range.y; double top_z = cos_lat * cos_theta * range.x + cos_lat * sin_theta * range.y + sin_lat * range.z; 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.w); double rate = range.Dot(range_rate) / range.w; /* * azimuth in radians * elevation in radians * range in km * range rate in km/s */ return CoordTopocentric(az, el, range.w, rate); } } // namespace libsgp4