Path: FormationFlying/Coord
% Two orbits are initialized with a small inclination difference. The orbits are propagated with Kepler's equations using RVOrbGen. The ECI position and velocity of each orbit is then transformed into the relative Hills frame. Since version 7. ------------------------------------------------------------------------ See also Constant, Plot2D, ECI2Hills, RVOrbGen ------------------------------------------------------------------------ % ------------------------------------------------------------------------------- Copyright (c) 2002 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------------
AC: ACData/ACTConstants FormationFlying: Coord/GetHillsMats FormationFlying: Transformation/ECI2Hills Orbit: OrbitCoord/SLR Orbit: OrbitMechanics/RVOrbGen SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/RV2El SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Math: Linear/Cross Math: Linear/Dot Math: Linear/DupVect Math: Linear/Mag
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