To intercept high-speed, highly maneuverable targets at mid-to-high altitudes, this paper explores disturbance-rejection guidance laws for missiles with canard/tail rudder control. By integrating the canard/tail rudder composite control method with disturbance-rejection guidance laws, we significantly enhance the maneuverability, manipulation ability, and guidance precision of missiles. The optimal control algorithm refines the canard/tail rudder distribution strategy, while real-time disturbance-rejection compensates for unknown disturbances. Simulations show that this approach improves target interception performance and hit probability.


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    Titel :

    On Disturbance-Rejection Guidance Laws for Missiles with Canard/Tail Rudder Control


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Yan, Liang (Herausgeber:in) / Duan, Haibin (Herausgeber:in) / Deng, Yimin (Herausgeber:in) / Zhao, Hongyu (Autor:in) / Xu, Shengli (Autor:in) / Ren, Yifan (Autor:in) / Yang, Ya (Autor:in) / Yin, Wei (Autor:in)

    Kongress:

    International Conference on Guidance, Navigation and Control ; 2024 ; Changsha, China August 09, 2024 - August 11, 2024



    Erscheinungsdatum :

    02.03.2025


    Format / Umfang :

    11 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






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