Requirements established in Douglas design study for stability augmentation system of 35,000-lb ducted fan VTOL aircraft; stabilization of VTOL aircraft resulted in design of Bang-Bang constant servo rate stability augmentation system; phase plane analysis; results of electronic analog computer study; system mechanization and operation; functional block diagram and servo control schematic; advantages; extension of technique.


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    Title :

    Application of Bang-Bang servo system to VTOL stability augmentation


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1962 VTOL-STOL



    Publication date :

    1962


    Size :

    9 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :