Path: Orbit/OrbitManeuver
% Computes the delta-V for a 2-burn transfer to a circular orbit at rF. The delta-Vs are at a. the initial orbit b. the final orbit -------------------------------------------------------------------------- Form: [deltaV, tOF, transfer] = OrbMnvrCircularize( rI, vI, gammaI, rF, mu ) -------------------------------------------------------------------------- ------ Inputs ------ rI (1,1) Initial radius vI (1,1) Initial velocity gammaI (1,1) Initial flight path angle (rad) rF (1,1) Final radius mu (1,1) Gravitational parameter ------- Outputs ------- deltaV (1,1) Delta-V data structure. .total (1,1) Total required delta-V .a (1,1) Delta-V at point a .b (1,1) Delta-V at point b .dVaHoriz (1,1) Horizontal portion of (a) .dVaVert (1,1) Vertical portion of (a) tOF (1,1) Time of flight --------------------------------------------------------------------------
Orbit: OrbitCoord/RV2AE SC: BasicOrbit/Nu2M SC: BasicOrbit/VOrbit Math: Linear/Mag
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