The purpose of this project was to provide a means for operating the ailerons, elevator, elevator trim, rudder, nosewheel steering, and brakes in the Triton primary flight trainer. The main design goals under consideration were to illustrate system and subsystem integration, control function ability, and producibility. Weight and maintenance goals were addressed.


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    Title :

    Cockpit Control System Conceptual Design


    Contributors:
    G. Meholic (author) / R. Brown (author) / M. Hall (author) / R. Harvey (author) / M. Singer (author)

    Publication date :

    1993


    Size :

    39 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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