Path: SCPro/ProSensors
% Demonstrate GPS navigation message model. This routine runs the receiver model using the navigation message and GPSOrbit. The satellites in view of the receiver are plotted at each step. ------------------------------------------------------------------------- See also GPSReceiverNav., Map, TimeGUI, Date2JD, RVFromKepler ------------------------------------------------------------------------- % -------------------------------------------------------------------------- Copyright 2003 Princeton Satellite Systems, Inc. All rights reserved. --------------------------------------------------------------------------
AerospaceUtils: Coord/IntersectPlanet SC: BasicOrbit/CP2I SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: BasicOrbit/OrbRate SC: BasicOrbit/RVFromKepler SC: Ephem/EOfE SC: Ephem/EarthNut SC: Ephem/EarthPre SC: Ephem/EarthRot SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/NutDelta SC: Ephem/ObOfE SC: Ephem/TruEarth SCPro: ProSensors/GPSOrbit SCPro: ProSensors/GPSReceiverNav SCPro: ProSensors/RangeMeasurement Common: CommonData/SwooshWatermark Common: GUIs/TimeGUI Common: General/CellToMat Common: General/CloseIfHandle 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/Dot Math: Linear/DupVect Math: Linear/Mag Math: MathUtils/R2P5 Math: Trigonometry/CosD Math: Trigonometry/SinD
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