Path: Orbit/OrbitMechanics
% Computes the semi-major axis given the mean orbit rate. Has a built-in demo with a plot. Since version 1. -------------------------------------------------------------------------- Form: a = N2A( n, mu ) -------------------------------------------------------------------------- ------ Inputs ------ n Mean orbit rate mu Gravitational constant (default is Earth) ------- Outputs ------- a Semi-major axis -------------------------------------------------------------------------- References: Bates, R.B. Fundamentals of Astrodynamics, pp. 185-187. --------------------------------------------------------------------------
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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