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SUPPORT SITE |
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Path: Orbit/OrbitCoord
% Computes v and r given a, e and nu. Also gives the time for each step. -------------------------------------------------------------------------- Form: [v, r, t] = AE2VR( a, e, nu, mu ) -------------------------------------------------------------------------- ------ Inputs ------ a (1,1) Semi major axis e (1,1) Eccentricity nu (1,n) True anomaly (rad) mu (1,1) Gravitational parameter (default = 3.98600436e5) ------- Outputs ------- v (1,n) Velocity r (1,n) Radius t (1,n) Time --------------------------------------------------------------------------
Common: Graphics/Plot2D Orbit: OrbitCoord/RPRA2AE SC: BasicOrbit/Nu2M
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