Path: AerospaceUtils/Coord
% Transform between selected coordinate frames and representations. The frames are: ECI Earth centered inertial ECR/EF Earth fixed LLR Geodetic latitude, longitude and altitude -------------------------------------------------------------------------- Form: x = CoordinateTransform( from, to, x, jD ) -------------------------------------------------------------------------- ------ Inputs ------ from (1,:) From (ECI, EF/ECR, LLR) to (1,:) To (ECI, EF/ECR, LLR) x (3,:) Vectors jD (3,1) Julian date ------- Outputs ------- xT (3,:) Vectors transformed --------------------------------------------------------------------------
AC: ACData/ACTConstants AerospaceUtils: Coord/ECIToEF AerospaceUtils: Coord/EFToLatLonAlt AerospaceUtils: Coord/LatLonAltToEF SC: Ephem/EOfE SC: Ephem/EarthNut SC: Ephem/EarthPre SC: Ephem/EarthRot SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/NutDelta SC: Ephem/ObOfE SC: Ephem/TruEarth SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/xSplashSmall Common: Database/Constant Common: General/DeleteCell Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2T Common: Time/JDToMidnight Common: Time/T2JD Math: Linear/Mag Math: Linear/Unit Math: MathUtils/R2P5 Math: Trigonometry/CosD Math: Trigonometry/SinD
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