Path: Orbit/OrbitCoord
% Convert semi-major axis & ecc. to velocity, altitude, flight path angle Since version 10. -------------------------------------------------------------------------- Form: [V,h,fpa] = AENuToVelAltFpa( a, e, nu, Rp, mu ) -------------------------------------------------------------------------- ------ Inputs ------ a (1,1) Semi-major axis e (1,1) Eccentricity nu (1,:) True anomaly (rad) Rp (1,1) Radius of planet (km) mu (1,1) Gravitational constant (km^3/s^2) ------- Outputs ------- V (1,:) Velocity (km/s) h (1,:) Altitude (km) fpa (1,:) Flight path angle (rad) --------------------------------------------------------------------------
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