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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

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


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Deng, Yimin (editor) / Zhao, Hongyu (author) / Xu, Shengli (author) / Ren, Yifan (author) / Yang, Ya (author) / Yin, Wei (author)

    Conference:

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



    Publication date :

    2025-03-02


    Size :

    11 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English






    Telescopic canard rudder mechanism

    XU QUAN / WANG BOLAN / XU SHENGLI et al. | European Patent Office | 2021

    Free access


    AIAA-2006-6569 Optimal Control Solution for Dual (Tail and Canard) Controlled Missiles

    Mracek, C. / Ridgely, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006