Properties are investigated of optimum processes of flight control of spacecraft when complete information about motion is available and when control is produced with the purpose of maintaining given values of certain functionals of the trajectory. Such functionals can be parameters of the trajectory characterizing conditions of encounter with a planet or another apparatus in outer space, or parameters determining spatial position of apparatus at a fixed moment of time.


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    Titel :

    Optimization of Flight Control of Spacecraft


    Beteiligte:
    A. K. Platonov (Autor:in) / A. A. Dashkov (Autor:in) / V. N. Kubasov (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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