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SUPPORT SITE |
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Path: SCPro/ProSensors
% GPS receiver model with navigation message model.
Failure mode is zero output.
See also GPSOrbit and RangeMeasurement.
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Form:
y = GPSReceiverNav( action, d )
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Inputs
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action (1,:) 'initialize' 'update' 'output' 'set failure'
'get default datastructure'
d (1,1) Depends on the action
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Outputs
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y (1,1) Depends on the action
The regular output is a structure:
.rGPS (3,n) Position of GPS satellites in view
.vGPS (3,n) Velocity of satellites
.range (1,n) Range to the satellites (km)
.rangeRate (1,n) Range rate (km/s)
.iD (1,n) ID of satellites in view
.nSatellites (1,1) Number of satellites in view
.message (:) GPS ephemeris message
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AerospaceUtils: Coord/IntersectPlanet Common: Time/Date2JD Common: Time/JD2T SC: BasicOrbit/OrbRate SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/TruEarth SCPro: ProSensors/GPSOrbit SCPro: ProSensors/RangeMeasurement
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