An active fault-tolerant flight control system design technique against control surface impairments is proposed here. The aircraft control surface impairments are modeled as a polytopic linear parameter varying (LPV) system. Relying on the existing control surface redundancy of the aircraft, both state feedback and static output feedback controllers are synthesized against various degrees of control surface impairments. Simulation examples of an aircraft subject to inner elevon impairments have been used to illustrate the design process and to demonstrate the effectiveness of the proposed method.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Fault-Tolerant Flight Control System Design Against Control Surface Impairments


    Beteiligte:
    Xiang Yu, (Autor:in) / Jin Jiang, (Autor:in)


    Erscheinungsdatum :

    2012-04-01


    Format / Umfang :

    2450939 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Fault Tolerant Flight Control

    Meir Pachter / Yih-Shiun Huang | AIAA | 2003


    FAULT TOLERANT AIRCRAFT FLIGHT CONTROL SYSTEM

    TELES FERREIRA JOÃO FILIPE / RIBAS GABRIEL OLIVEIRA | Europäisches Patentamt | 2022

    Freier Zugriff

    Fault-Tolerant Flight Control Using One Aerodynamic Control Surface

    Venkataraman, Raghu / Seiler, Peter | AIAA | 2018


    FAULT TOLERANT AIRCRAFT FLIGHT CONTROL SYSTEM

    TELES FERREIRA JOÃO FILIPE / RIBAS GABRIEL OLIVEIRA | Europäisches Patentamt | 2024

    Freier Zugriff

    Fault tolerant fiber optic flight control system

    Schwabenland, B. / Stipanovich, J. / Smith, B. et al. | Tema Archiv | 1990