Path: Orbit/OrbitCoord
% Generates an array of true anomalies. -------------------------------------------------------------------------- Form: [nu, dT, t] = TrueAnomalySpacing( e, nu0, n, duration, nS, eTol ) -------------------------------------------------------------------------- ------ Inputs ------ e (1,1) Eccentricity nu0 (1,1) Initial true anomaly (rad) n (1,1) Mean orbit rate (rad/s) duration (1,1) Duration of array (sec) nS (1,1) Total number of samples eTol (1,1) Tolerance on e (circular orbit) ------- Outputs ------- nu (1,:) True anomalies dT (1,:) Time steps t (1,:+1) Time vector --------------------------------------------------------------------------
SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuAbs SC: BasicOrbit/M2NuPb SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/DupVect Math: Trigonometry/UnwrapPhase
Back to the Orbit Module page