Fixed base and piloted simulation studies were conducted to evaluate control systems for a STOL tactical transport equipped with vectored thrust. Unaugmented aircraft flying qualities were found to be unacceptable. However, an augmented control system configuration was found to give excellent flying qualities and satisfactory behavior following engine or control system component failure. The present flying qualities standard for STOL aircraft, MIL-F-83300, was reviewed and several changes are suggested. (Author)


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    Title :

    STOL Tectical Aircraft Investigation. Volume V. Part II. Flight Control Technology: Piloted Simulation of a Medium STOL Transport with Vectored Thrust Mechanical Flaps


    Contributors:

    Publication date :

    1973


    Size :

    246 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English