Osculating/Mean Orbital Element Conversion (C version) (OSMEANC) is a C-language computer program that performs precise conversions between osculating and mean classical orbital elements. OSMEANC can be used for precise design of spacecraft missions and maneuvers and precise calculation of planetary orbits. The program accounts for the full complexity of gravitational fields, including aspherical and third-body effects.


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    Title :

    Conversion Between Osculating and Mean Orbital Elements


    Contributors:


    Publication date :

    2006-11-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Conversion Of Osculating Orbital Elements To Mean Orbital Elements

    Der, G. / Danchick, R. / Goddard Space Flight Center | British Library Conference Proceedings | 1996