Path: FormationFlying/Transformation
% Transforms mean orbital elements to osculating orbital elements.
Element vector in standard form: [a,i,W,w,e,M]
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Form:
el_mean = Mean2Osc(el_osc);
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Inputs
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el_mean (1,6) mean orbital elements
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Outputs
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el_osc (1,6) osculating orbital elements
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References: Terry Alfriend, Texas A&M University, 2001
Rich Burns, 1999
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SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/DupVect
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