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Path: SpacecraftEstimation/SensorMeas
% GPS range and range rate model for use with UKF.
If d.noise is entered it will add Gaussian noise to the values.
Since version 2014.1
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Form:
y = MeasGPS( x, d )
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Inputs
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x (6,1) State [r;v]
d (1,1) Filter data structure
.jD (1,1) Julian date
.jD0 (1,1) Initial Julian Date
.noise (2,1) [range;range rate] noise
.rE (1,1) Earth radius
.rRef (1,1) Reference length
.hMin (1,1) Minimum altitude for GPS visibility
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Outputs
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y (2*n,1) GPS range and range rate
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AerospaceUtils: Coord/IntersectPlanet Math: Linear/Cross Math: Linear/Mag SC: BasicOrbit/CP2I SC: BasicOrbit/OrbRate
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