A fixed compensation design theory is presented for achieving flight control performance, despite one or more simultaneous failures, hardover and varying flight conditions. No identification is used. The theory is a natural extension of Quantitative Feedback Theory (QFT) for uncertain systems, and clearly reveals the cost of feedback needed. This enables the designer to make intelligent trade-offs between fixed compensation, scheduling and identification-adaptation. Identification, when it is necessary, can be done more slowly and accurately if a QFT design is made so the system in at least stable over many simultaneous failures. The theory is applied to the YF16CCV model with elevators and flaperons for pitch and roll rate control.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    YF16CCV flight control system reconfiguration design using quantitative feedback theory


    Additional title:

    Rekonfiguration des YF16CCV Flugsteuerungssystems, Entwicklung mit der quantitativen Rueckkopplungs-Theorie


    Contributors:
    Horowitz, I. (author) / Arnold, P.B. (author) / Houpis, C.H. (author)


    Publication date :

    1985


    Size :

    8 Seiten, 14 Bilder, 12 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English