The theory of vertical fall in the atmosphere was investigated as applied to an unmanned return spacecraft for various cases of ratio of the initial and quasi-steady-state velocities of fall. The modeling of the braking process, which is the numerical integration of the system from the first part of this paper, is presented. The landing dynamics simulates the action of an unmanned return spacecraft in flight.


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    Titel :

    Adaptive Algorithm for Controlling the Soft Vertical Landing of an Unmanned Return Spacecraft. II


    Weitere Titelangaben:

    Russ. Aeronaut.


    Beteiligte:

    Erschienen in:

    Russian Aeronautics ; 64 , 2 ; 189-196


    Erscheinungsdatum :

    2021-04-01


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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