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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Qualification of HiMAT flight systems


    Beteiligte:
    Myers, A. F. (Autor:in) / Sheets, S. G. (Autor:in)

    Kongress:

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


    Erscheinungsdatum :

    1980-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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


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


    HiMAT aerodynamic design and flight test experience

    MATHENY, N. / PANAGEAS, G. | AIAA | 1981