Path: Orbit/OrbitMechanics
% Monte-Carlo orbit simulation. Type RandomOrbit for a demo with 2008 AE9 Since version 11. -------------------------------------------------------------------------- Form: [r1S, v1S, rN, vN] = RandomOrbit( el, el1S, t, mu, n ) -------------------------------------------------------------------------- ------ Inputs ------ elI (1,6) Elements vector [a,i,W,w,e,M] el1S (1,6) Gaussian noise vector [a,i,W,w,e,M] t (1,1) Times from 0 to (sec) mu (1,1) Gravitational parameter ------- Outputs ------- r1S (3,1) Mean position 1 sigma (km) v1S (3,1) Mean velocity 1 sigma (km) rN (3,1) Nominal position (km) vN (3,1) Nominal velocity (km) --------------------------------------------------------------------------
AC: ACData/ACTConstants 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: 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/DupVect Math: Linear/Mag
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