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Path: Orbit/Demos/OrbitControl
% Demonstrates the Lambert targeting function DVTarget. The selected time of flight drastically affects the resulting delta-V, from 181 m/s to 23 km/sec. ------------------------------------------------------------------------- Reference: Vallado 2nd edition, p.476 and Fig. 7-20 ------------------------------------------------------------------------- See also Plot3D, TitleS, XLabelS, YLabelS, Mag, DVTarget, LambertTOF, RV2El, RVFromKepler ------------------------------------------------------------------------- % -------------------------------------------------------------------------- Copyright 2003 Princeton Satellite Systems, Inc. All rights reserved. --------------------------------------------------------------------------
Common: Graphics/NewFig Common: Graphics/Plot3D Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Math: Linear/Mag Orbit: OrbitControl/DVTarget Orbit: OrbitMechanics/LambertTOF SC: BasicOrbit/RV2El SC: BasicOrbit/RVFromKepler
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