Substantial progress has been made towards designing a full envelope, decoupled helicopter flight control system with initial designs having been successfully 'flown' on the RAE Bedford flight simulator. Results have shown that the mu -synthesis controller design method offers significant performance robustness to changes in the system operating point when compared to methods which do not incorporate a model of system uncertainty into the design process. Further results show how controller conditioning can be used to prevent unnecessary degradation of performance, for example through integral windup, during actuator saturation.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    The use of mu-synthesis in full envelope, helicopter flight control system design


    Additional title:

    Die Anwendung der mu-Synthese zum Entwurf eines Hubschrauberflugregelsystems


    Contributors:
    Maclay, D. (author) / Williams, S.J. (author)

    Published in:

    Publication date :

    1991


    Size :

    6 Seiten, 4 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Development of Full Flight Envelope Helicopter Simulation Using System Identification

    Zivan, L. / Tischler, M. B. / AHS International | British Library Conference Proceedings | 2007


    Active model based predictive control for unmanned helicopter in full flight envelope

    Song, Dalei / Qi, Juntong / Han, Jianda et al. | Tema Archive | 2010