Path: SC/Sensor
% Gives the location of the GPS satellites at JD.
Choice of Earth-fixed or ECI reference frames.
Type GPSSatellite for a demo.
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Forms:
[r, v] = GPSSatellite( jD )
[r, v] = GPSSatellite( jD, coord )
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Inputs
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jD (1,1) Julian Date
coord (1,:) 'ef' or 'eci' (eci is the default)
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Outputs
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r (3,24) Satellite locations
v (3,24) Satellite velocity
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Reference: Kayton, M. and W. R. Fried. (1997.) "Avionics Navigation
Systems," John Wiley & Sons.
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