Flight verification of a primary flight control system, designed to control the unstable HiMAT aircraft is presented. The initial flight demonstration of a maneuver autopilot in the level cruise mode and the gathering of a limited amount of airspeed calibration data.


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    Title :

    HiMAT highly maneuverable aircraft technology, flight report


    Publication date :

    1982-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English