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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    Titel :

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


    Beteiligte:
    N. L. Sokolov (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch