A method is proposed for calculating the atmospheric entry maneuvers of a spacecraft. Errors are evaluated for calculations of spacecraft with zero and constant values of lift-drag ratio, as well as for problems of optimal control. Particular attention is given to the determination of the trajectory parameters of the ballistic descent of spacecraft from earth-satellite orbit.


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    Title :

    Approximate Analytic Method of Calculating Spatial Maneuvers of Spacecraft in Atmosphere. Abstract Only


    Contributors:

    Publication date :

    1989


    Size :

    1 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English