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SUPPORT SITE |
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Path: Orbit/OrbitCoord
% Transform Sun-Earth-Moon rotating (SEMR) state to the heliocentric frame. The SEMR coordinate frame is +x pointing at the earth along the sun-earth line. +z normal to the sun-earth plane and +y completing the set. Type TransformSEMRToHelio for a demo -------------------------------------------------------------------------- Form: [rHelio,vHelio,mRot] = TransformSEMRToHelio( jD, rSEMR, vSEMR ) -------------------------------------------------------------------------- ------ Inputs ------ jD (1,:) Julian date (days) rSEMR (3,:) Position vector in SEMR frame vSEMR (3,:) Velocity vector in SEMR frame ------- Outputs ------- rHelio (3,:) Position vector in heliocentric frame vHelio (3,:) Velocity vector in heliocentric frame mRot (3,3) Rotation matrix -------------------------------------------------------------------------- See also TransformSEMRToECI and SunV2 --------------------------------------------------------------------------
Common: Database/Constant Common: Time/Date2JD Math: Linear/Mag Orbit: OrbitCoord/TransformECIToSEMR Orbit: OrbitCoord/TransformSEMRToECI SC: Ephem/SunV2
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