Path: Orbit/OrbitMechanics
% Computes the longitudinal motion due to an acceleration a -------------------------------------------------------------------------- Form: [lon, lond] = LonMot( lon0, lond0, a, t ) -------------------------------------------------------------------------- ------ Inputs ------ lon0 Initial longitude lond0 Initial longitude rate a Acceleration t Time ------- Outputs ------- lon Longitude (rad) lond Longitude rate --------------------------------------------------------------------------
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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