Path: Orbit/OrbitMechanics
% Position and velocity relative to the target
Also returns latitude, longitude and altitude.
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Form:
d = LunarRelativeState(x,jD,rTarget)
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Inputs
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x (20,1) State vector [r;v;..] (km,km/s)
jD (1,1) Julian date
rTarget (3,1) Target position in the lunar frame (km)
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Outputs
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d (.) Data structure for the output
.lat (1,1) Latitude (deg)
.lon (1,1) Longitude (deg)
.alt (1,1) Altitude (km)
.r (3,1) Relative position (km)
.v (3,1) Relative velocity (km/s)
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AerospaceUtils: Coord/EFToLatLonAlt SC: Ephem/MoonRot Math: Linear/Cross
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