A set modified equinoctial orbit elements
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Từ khóa
Tài liệu tham khảo
Cefola, P.J.: 1972,Equinoctial Orbit Elements-Application to Artificial Satellite Orbits, AIAA preprint 72-937.
Cornelisse, J.W., Shöyer, H.F.R., and Wakker, K.F.: 1979,Rocket Propulsion and Spacecraft Dynamics, Pitman.
Kaula, W.M.: 1966,Theory of Satellite Geodesy, Blaisdell.
Roth, E.A.: 1970,ZAMP 30 (2), 315?325.