Path: Orbit/OrbitCoord
% Convert the standard orbital element set into an Alfriend orbital element set
[a,i,W,w,e,M] -> [a,th,i,q1,q2,W]
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Form:
ela = El2Alfriend( el, nu )
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Inputs
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el (:,6) Standard orbital element set [a,i,W,w,e,M]
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Outputs
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ela (:,6) Alfriend orbital element set [a,th,i,q1,q2,W]
where: th = true latitude
q1 = e*cos(w)
q2 = e*sin(w)
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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/WrapPhase
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