Path: Missions/LunarLanding
% Lunar surface landing target -------------------------------------------------------------------------- Form: r = LunarTarget( x, jD, downrange ) -------------------------------------------------------------------------- ------- Inputs ------- x (20,1) State vector [r;v;..] (km,km/s) jD (1,1) Julian date downrange (3,1) Downrange distance ------- Outputs ------- r (3,1) Landing spot in the lunar fixed frame --------------------------------------------------------------------------
SC: Ephem/MoonRot Math: Linear/Unit
Back to the Missions Module page