This paper aims to demonstrate the effectiveness of a fault-tolerant flight control method by using simple adaptive control (SAC) with PID controller.

    Design/methodology/approach

    Numerical simulations and flight tests are executed for pitch angle and roll angle control of research aircraft MuPAL-α under the following fault cases: sudden reduction in aileron effectiveness, sudden reduction in elevator effectiveness and loss of longitudinal static stability.

    Findings

    The simulations and flight tests reveal the effectiveness of the proposed SAC with PID controller as a fault-tolerant flight controller.

    Practical implications

    This research includes implications for the development of vehicles’ robustness.

    Originality/value

    This study proposes novel SAC-based flight controller and actually demonstrates the effectiveness by flight test.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Flight test of fault-tolerant flight control system using simple adaptive control with PID controller


    Beteiligte:
    Matsuki, Hidenobu (Autor:in) / Nishiyama, Taishi (Autor:in) / Omori, Yuya (Autor:in) / Suzuki, Shinji (Autor:in) / Masui, Kazuya (Autor:in) / Sato, Masayuki (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    02.01.2018


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Flight Test of Fault-Tolerant Flight Control System using Simple Adaptive Control with PID Compensator (AIAA 2013-5210)

    Omori, Y. / Suzuki, S. / Masui, K. et al. | British Library Conference Proceedings | 2013




    FAULT-TOLERANT FLIGHT CONTROL SYSTEM WITH SIMPLE ADAPTIVE CONTROL CONSIDERING PILOT INPUT

    Takase, R. / Entzinger, J. O. / Suzuki, S. | British Library Conference Proceedings | 2018