An account is given of flight control system performance results for the X-29A forward-swept wing 'Advanced Technology Demonstrator' fighter aircraft, with attention to its software and hardware components' achievement of the requisite levels of system stability and desirable aircraft handling qualities. The Automatic Camber Control Logic is found to be well integrated with the stability loop of the aircraft. A number of flight test support software programs developed by NASA facilitated monitoring of the X-29A's stability in real time, and allowed the test team to clear the envelope with confidence.


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    Titel :

    X-29A flight control system performance during flight test


    Beteiligte:
    Chin, J. (Autor:in) / Chacon, V. (Autor:in) / Gera, J. (Autor:in)

    Erscheinungsdatum :

    01.09.1987


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    X-29A flight control system performance during flight test

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    Gemini flight control system performance during second unmanned flight

    Hanaway, J.F. / Carley, R.R. / Vernon, J.A. | Engineering Index Backfile | 1965


    Gemini flight control system performance during the second unmanned flight.

    Carley, R. R. / Hanaway, J. F. / Vernon, J. A. | NTRS | 1965


    Gemini Flight Control System Performance during the Second Unmanned Flight

    Vernon, J. A. / Hanaway, John F. / Carley, R. R. | SAE Technical Papers | 1965