Path: Orbit/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. --------------------------------------------------------------------------