A fuzzy set-point weighting proportional-integral-derivative (PID) controller is applied in the development of the flight control system for a two-dimensional differential geometric (DG) guidance and control system, whose function is to guarantee the achieved angle of attack (AOA) and track the commanded AOA efficiently. In particular, a Lyapunov stability criterion is introduced to study the relation between the stability and the output of the fuzzy inference system, and a genetic algorithm is utilised to tune the PID gains in the simulations so as to show the full potentiality of the proposed control scheme. The results demonstrate that the designed controller yields a fast-responding and stable system that is robust to parameter variations. Moreover, the DG guidance law is viable and effective in a realistic missile defence engagement.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Fuzzy PID controller for 2D differential geometric guidance and control problem


    Beteiligte:
    Li, C.Y. (Autor:in) / Jing, W.X. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2007


    Format / Umfang :

    8 Seiten, 25 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch





    Iterative solution to differential geometric guidance problem

    Li, Chaoyong / Jing, Wuxing / Wang, Hui et al. | Emerald Group Publishing | 2006


    New Differential Geometric Guidance Strategies for Impact-Time Control Problem

    Wang, Pengyu / Guo, Yanning / Ma, Guangfu et al. | AIAA | 2019


    Analytical solution to 3D differential geometric guidance problem

    Chaoyong Li, / Wuxing Jing, / Hui Wang, et al. | IEEE | 2006