Path: FormationFlying/Utility
% Generate an orbit by propagating Keplerian elements with impulsive delta-vs. Since version 7. -------------------------------------------------------------------------- Form: [r, v] = RVOrbGenDV( el, t, dV, dVTime ) -------------------------------------------------------------------------- ------ Inputs ------ elI Elements vector [a,i,W,w,e,M] or structure t Times from 0 to ? (sec) dV Array of 3xN delta-v's to be applied (Hills frame) [km/sec] dVTime Array of 1xN times at which delta-v's are applied [sec] ------- Outputs ------- r Position vectors for times t v Velocity vectors for times t el Times at which r and v are calculated --------------------------------------------------------------------------
FormationFlying: Coord/GetHillsMats 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 Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT 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/DupVect Math: Linear/Mag
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