Path: Orbit/OrbitManeuver
% Compute the maneuver envelope for a spacecraft rotating around another. -------------------------------------------------------------------------- Form: [p, r] = ManeuverEnvelope( f, m ) -------------------------------------------------------------------------- ------ Inputs ------ f (:,1) Available force m (1,1) Mass ------- Outputs ------- p (1,:) Period r (1,:) Corresponding radius --------------------------------------------------------------------------
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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