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updated 1 year ago

Convert Keplerian Orbital Elements to a State Vector by Darin Koblick

Darin Koblick

Convert orbital elements to a state vector, or a state vector back to orbital elements. (keplerian, orbital elements, aerospace)

orb2rv(p,e,i,O,o,nu,truLon,argLat,lonPer,mu)

rv2orb(r,v,mu)

test_orb2rv.m

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updated 2 years ago

Two Line Element by Small Satellites

Small Satellites

Example how to open and read two line element file and output six orbital elements (aerospace, two line element, tle)

Two_line_Element.m

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updated 2 years ago

Classical Orbital Elements GUI by Anders Edfors Vannevik

Anders Edfors Vannevik

Visualize Classical Orbital Elements (aerospace, aeronautics, aerodef)

Classical Orbital Elements GUI

coe_gui(varargin)

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