Feedback control for flexible landing approach profiles of rotary wing aircraft was investigated. The feedback control circuit, in which the state vector contains 8 variables, is described. Solutions to the linearized state equation are illustrated by examples with results of simulation, during which straight-line, curved, and spatially curved approaches were investigated.


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    Titel :

    Control Technique in Steep Approach of Rotary Wing Aircraft Regelungstechnik bei Steilanfluegen von Drehflueglern


    Beteiligte:
    W. Kubbat (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







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