Path: LunarMissions/LunarMission
% Computes visibility of a satellite in lunar orbit. Uses the Clementine surface model. The orbit is in the inertial frame but lunar centric. Type LunarVisibility for a demo. -------------------------------------------------------------------------- Form: kVis = LunarVisibility( lat, lon, jD0, r, t, nH ) -------------------------------------------------------------------------- ------ Inputs ------ lat (1,1) Latitude of the ground target (rad) lon (1,1) Longitude of the ground target (rad) jD0 (1,1) Julian data of start (days) r (3,:) ECI frame orbit (rad) t (1,:) Times corresponding to points in r (s) nH (1,1) Number of harmonics in the surface model (72 maximum) ------- Outputs ------- kVis (1,:) 1 if the satellite is visible, 0 if not -------------------------------------------------------------------------- See also RSHMoon. --------------------------------------------------------------------------
AerospaceUtils: Coord/LatLonToR AerospaceUtils: Coord/U2RADec Orbit: OrbitCoord/RPRA2AE Orbit: OrbitMechanics/RVOrbGen SC: Ephem/LoadLunarTopography SC: Ephem/MoonRot SC: Ephem/RSHMoon Common: Database/Constant Common: General/Watermark Common: Graphics/Map Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/TimeLabl Common: Time/Date2JD Math: Linear/Mag Math: Linear/Unit
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