Path: Plotting/Derivation Functions
% Transform ECI position and velocity into orbital elements. -------------------------------------------------------------------------- Form: out = RV2ElDPT( varargin ) -------------------------------------------------------------------------- ------ Inputs ------ varargin (:) Variable number of inputs, raw simulation data. ------- Outputs ------- out (1,:) Derived output data. --------------------------------------------------------------------------
SC: BasicOrbit/E2M SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/RV2El Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/Cross Math: Linear/DupVect Math: Linear/Mag
Back to the Plotting Module page