Principles of gust alleviation; technique employs high response, servo driven, lift modifying control surfaces, and wind flow sensor or accelerometer to provide signal representing gust velocity profile as input command signal to gust alleviator; integration in flight control system; schematics and block diagrams; system which integrates human pilot, autopilot, gust alleviator, and rigidity augmentor.


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    Titel :

    Integration of gust alleviators in flight control systems


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Andrew, G.M. (Autor:in) / Gardner, F.H. (Autor:in)

    Kongress:

    SAE Meeting ; 1961 Control equipment



    Erscheinungsdatum :

    1961


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Integration of Gust Alleviators in Flight Control Systems

    Gardner, F. H. / Andrew, G. M. | SAE Technical Papers | 1961



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    Croom, Delwin R. / Shufflebarger, C. C. / Huffman, Jarrett K. | TIBKAT | 1956



    Atmospheric Flight Gust Loads Analysis

    M. C. Kim / A. M. Kabe / S. S. Lee | AIAA | 2000