The different model matching approaches (Exact, PIM (Pseudo-Inverse Method), NPIM (Modified Pseudo-Inverse Method)) are analyzed for the fault tolerant control of the short-period mode of the longitudinal model of the Boeing 747 aircraft. To overcome the drawbacks of the PIM and MPIM approaches, a new philosophy is proposed for the model matching problem, namely to use a set of admissible models instead of trying to best approximate a single reference one. The application shows the benefits associated with using this approach.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Fault tolerant control of the Boeing 747 short-period mode using the admissible model matching technique


    Additional title:

    Fehlertolerante Regelung einer Boeing 747 in Kurzdauermodus mittels Modellanpassungsmethode


    Contributors:


    Publication date :

    2006


    Size :

    6 Seiten, 1 Bild, 3 Tabellen, 19 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English






    Reconfigurable Fault Tolerant Control of a Boeing 747 Using Subspace Predictive Control AIAA Paper

    Hallouzi, R. / Verhaegen, M. | British Library Conference Proceedings | 2007



    Incremental Sliding-Mode Fault-Tolerant Flight Control

    Wang, Xuerui / Kampen, Erik-Jan van / Chu, Qiping et al. | AIAA | 2018