The article discusses some of the problems involved in bringing a winged space apparatus down at a landing site from a circular orbit. It discusses longitudinal and lateral control of the aircraft in the descent process. A system for the automatic control of the space apparatus in the descent process is described, with emphasis on the effect of various disturbances.


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    Titel :

    Nonlinear Laws of Control of a Gliding Winged Space Apparatus in Coming Out of Circular Orbit onto a Runway


    Beteiligte:
    V. S. Vedrov (Autor:in) / G. P. Vladychin (Autor:in) / A. A. Kondratov (Autor:in) / G. L. Romanov (Autor:in) / V. M. Shlaginov (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    24 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch