Numerical integration for continuously thrusting spacecraft optimal trajectory, considering rectangular Cartesian and polar cylindrical coordinates characteristics


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    Title :

    Coordinate system influence on the regularized trajectory optimization problem


    Contributors:

    Conference:

    ASTRODYNAMICS CONFERENCE ; 1969 ; PRINCETON, NJ, US


    Publication date :

    1971-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :