The results of a feasibility study and preliminary design for active control research and validation using the Total In-Flight Simulator (TIFS) aircraft are documented. Active control functions which can be demonstrated on the TIFS aircraft and the cost of preparing, equipping, and operating the TIFS aircraft for active control technology development are determined. It is shown that the TIFS aircraft is as a suitable test bed for inflight research and validation of many ACT concepts. (Author)


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    Title :

    Study for Active Control Research and Validation Using the Total in-Flight Simulator (Tifs) Aircraft


    Contributors:
    R. T. N. Chen (author) / H. Daughaday (author) / D. Andrisani (author) / R. D. Till (author) / N. C. Weingarten (author)

    Publication date :

    1975


    Size :

    164 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English