Path: SC/Ephem
% The position vectors, gravitational parameters and velocity for the planets.
The frame is centered on the Earth-Moon Barycenter and the plane is
ecliptic, i.e. xy-plane is the mean earth's orbital plane. d cannot
be empty on initialize.
Type PlanetPositionEMBarycenter for a demo
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Form:
[rB,vB,mu] = PlanetPositionEMBarycenter( action, d )
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Inputs
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action (1,:) 'initialize' or 'update'
d (1,n) Julian date (days) for 'update' or planet ids (1-9)
for initialize
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Outputs
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rB (3,n) Planetary position vectors
vB (3,n) Velocity vectors
mu (1,n) Corresponding gravitational parameters
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SC: Ephem/CEcl2Eq SC: Ephem/InterpolateState SC: Ephem/PlanetPosJPL SC: SCData/bin2000 Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000
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