Robust and early detection of oscillatory failures in the electrical flight control system of an aircraft is a crucial issue. Oscillatory failures, if not detected and passivated in time, can lead to strong interactions with loads and aeroelasticity and may potentially lead to structural damages. A nonlinear observer-based solution to detect such failures with small amplitude at a very early stage is presented. The stability and convergence proofs are given and experimental results with real A380 flight data are presented.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    A Nonlinear Observer-Based Strategy for Aircraft Oscillatory Failure Detection: A380 Case Study


    Contributors:


    Publication date :

    2011-10-01


    Size :

    2580713 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    A Nonlinear Observer-Based Strategy for Aircraft Oscillatory Failure Detection: A380 Case Study

    Alcorta-Garcia, E. / Zolghadri, A. / Goupil, P. | Tema Archive | 2011



    Aircraft - Flying the A380

    Online Contents | 2012


    A380 Aircraft Test Campaign

    Iannarelli, F. / Serrand, A. / Society of Flight Test Engineers | British Library Conference Proceedings | 2007


    A380 aircraft safety process

    Lawrence, B. | IET Digital Library Archive | 2006