Path: LunarMissions/LunarCoord
% Transform pos. and vel. from Earth Moon barycenter rotating frame to ECI
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
TransformEMBRToECI
for a demo
Since version 10.
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Form:
[xECI,vECI,m] = TransformEMBRToECI( xEMBR, jD )
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Inputs
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jD (1,:) Julian date (days)
rEMBR (3,:) Position vector in EMBR frame
vEMBR (3,:) Velocity vector in EMBR frame
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Outputs
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rECI (6,:) Position vector in ECI frame
vECI (6,:) Velocity vector in ECI frame
m {:} Rotation matrix
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Interplanetary: ThreeBody/CRTBPRHS LunarMissions: LunarCoord/ECIToEarthMoonRot Common: Database/Constant Common: Graphics/Plot3D Common: Time/JD2000
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