The highly maneuverable aircraft technology (HiMAT) remotely piloted research vehicle is discussed with emphasis on the advanced composite and metallic structures, digital fly-by-wire controls, and digitally implemented integrated propulsion control systems. Techniques used to qualify the systems for flight are examined. Computation and simulation of the HiMAT system are investigated in relation to Cyber-Varian simulation. The techniques used in flight qualification are complicated by ground based flight critical systems and severe onboard volume constraints imposed by the scale design.


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    Title :

    Qualification of HiMAT flight systems


    Contributors:

    Conference:

    Annual Technical Symposium of The Association for Unmanned Vehicle Systems ; 1980 ; Dayton, OH


    Publication date :

    1980-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    HiMAT onboard flight computer system architecture and qualification

    MYERS, A. F. / EARLS, M. R. / CALLIZO, L. A. | AIAA | 1983


    HiMAT onboard flight computer system architecture and qualification

    Myers, A. F. / Earls, M. R. / Callizo, L. A. | NTRS | 1983


    HiMAT onboard flight computer system architecture and qualification

    MYERS, A. / EARLS, M. / CALLIZO, L. | AIAA | 1981


    HiMAT onboard flight computer system architecture and qualification

    Myers, A. F. / Earls, M. R. / Callizo, L. A. | NTRS | 1981