Solutions of satellite orbit problem are obtained that do not exhibit singularities at critical inclination angle; series representations are obtained, their regions of convergence exhibited, and quantitative measures of their speeds of convergence provided for use in numerical computations.


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    Title :

    Critical inclination problem in satellite orbit theory


    Additional title:

    NASA -- Tech Report


    Contributors:


    Publication date :

    1962


    Size :

    66 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :





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