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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    Title :

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


    Contributors:
    W. Kubbat (author)

    Publication date :

    1973


    Size :

    26 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







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