Path: SCPro/ProSensors
% 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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SC: BasicOrbit/CP2I SC: BasicOrbit/OrbRate SC: BasicOrbit/RVFromKepler SC: Ephem/EOfE SC: Ephem/EarthNut SC: Ephem/EarthPre SC: Ephem/EarthRot SC: Ephem/EarthRte SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/NutDelta SC: Ephem/ObOfE SC: Ephem/TruEarth Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Ellipsd Common: Graphics/Map Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/Plot3D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2T Common: Time/JDToMidnight Math: Linear/Cross Math: Linear/DupVect Math: MathUtils/R2P5 Math: Trigonometry/CosD Math: Trigonometry/SinD
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