Generally, high performance requirements in terms of better efficiency (reduction in fuel consumption) and maneuverability, impose intrinsic instability on the aircraft. Then a Stability Augmentation System is required for its stabilization. Moreover, the aircraft must be safely controllable without any exceptional piloting skill. The requirements of stability and control are referred in literature as handling qualities. According to handling quality specifications, a feedback controller must be designed with robustness criteria with respect to flight conditions and sensor failure. A new design procedure of feedback controllers which allows the achievement of simultaneous stabilization, and provides some kind of fault tolerance with respect to sensor failure, are proposed. An application to the F4-E military aircraft is also presented.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Parameter Space Design of Robust Flight Control Systems


    Contributors:
    A. Cavallo (author) / G. Demaria (author) / L. Verde (author)

    Publication date :

    1990


    Size :

    13 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Robust flight control systems - A parameter space design

    CAVALLO, ALBERTO / DE MARIA / GIUSEPPE et al. | AIAA | 1992


    U-parameter robust flight control design

    Lin, Chih-Min / Tai, Ruey-Shih | AIAA | 1995


    U-Parameter Robust Flight Control Design

    Lin, C.-M. | Online Contents | 1995


    Parameter Space Design of Robust Control Systems

    Ackermann, J. | German Aerospace Center (DLR) | 1980

    Free access

    Robust Flight Control Design for Linear Systems with Real Parameter Uncertainty

    Devarakonda, Nagini / Sar, Preeti / Yedavalli, Rama K. | AIAA | 2015