Path: Orbit/OrbitCoord
% Transform ECI pos. and vel. to Earth Moon barycenter rotating frame. The EMBR coordinate frame is +x pointing at the earth along the earth-moon line. +z normal to the earth moon plane and +y completing the set. Uses MoonV1. Computes the plane by looking at the moon vector at jD(k) and then 1 day later. Type TransformECIToEMBR for a demo Since version 10. -------------------------------------------------------------------------- Form: [rEMBR,vEMBR,m] = TransformECIToEMBR( jD, rECI, vECI ) -------------------------------------------------------------------------- ------ Inputs ------ rECI (6,:) Position vector in ECI frame vECI (6,:) Velocity vector in ECI frame jD (1,:) Julian date (days) ------- Outputs ------- rEMBR (6,:) Position vector in EMBR frame vEMBR (6,:) Velocity vector in EMBR frame m {:} Rotation matrix --------------------------------------------------------------------------
Common: Database/Constant Common: Graphics/Plot3D Common: Time/JD2000 Orbit: OrbitCoord/ECIToEarthMoonRot
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