Path: FormationFlying/Transformation
% Compute standard differential elements from Alfriend differential elements. Since version 7. -------------------------------------------------------------------------- Usage: [dEl,T] = DeltaEl2Alfriend( e, w, M, dElA ); -------------------------------------------------------------------------- ------ Inputs ------ e (1) Eccentricity w (1) Argument of perigee [rad] M (1) Mean anomaly [rad] dElA (1,6) Orbital element differences [a,th,i,q1,q2,W] ------- Outputs ------- dEl (1,6) Orbital element differences [a,i,W,w,e,M] T (6,6) Transformation matrix --------------------------------------------------------------------------
SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb 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
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