Path: Orbit/OrbitMechanics
% Computes the mean orbit rate for an elliptic orbit -------------------------------------------------------------------------- Form: omegaMean = MeanMotn( a, mu ) -------------------------------------------------------------------------- ------ Inputs ------ a Semi-major axis mu Gravitational constant ------- Outputs ------- omegaMean mean orbit rate --------------------------------------------------------------------------
Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
Back to the Orbit Module page