A microcomputer-based integration of aircraft design disciplines has been applied theoretically to sailplane, microwave-powered aircraft, and High Altitude Long-Endurance (HALE) aircraft configurational definition efforts. Attention is presently given to the further development of such integrated-discipline approaches through the incorporation of AI techniques; these are then applied to the aforementioned case of the HALE. The windFrame language used, which is based on HyperTalk, will allow designers to write programs using a highly graphical, user interface-oriented environment.


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    Titel :

    Development of a microcomputer based integrated design system for high altitude long endurance aircraft


    Beteiligte:
    Hall, David W. (Autor:in) / Rogan, J. Edward (Autor:in)


    Erscheinungsdatum :

    1989-04-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    High Altitude Long Endurance Aircraft Design Studies

    Venkayya, V. B. / Tischler, V. A. / North Atlantic Treaty Organization | British Library Conference Proceedings | 1993



    Unmanned high altitude long-endurance aircraft

    PATTERSON, CHARLES | AIAA | 1989