Path: Orbit/OrbitManeuver
% Computes the optimal circular capture radius and delta-v. This can be used for heliocentric to planetary captures or moon captures. Since version 1. -------------------------------------------------------------------------- Form: [dV, rP] = DVOCCapt( muS, muP, r, v ) -------------------------------------------------------------------------- ------ Inputs ------ muS (1,1) Gravitational parameter of the central body muP (1,1) Gravitational parameter of the target body r (1,1) Target body orbit radius referenced to the center v (1,:) The central body velocity of the spacecraft ------- Outputs ------ dV (1,:) Minimum delta-v rP (1,:) Optimal circular radius about the target --------------------------------------------------------------------------
Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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