A cooperative trajectory shaping guidance law is proposed to address the problem of cooperative attack stationary target of multiple cruise missiles with certain tactical requirement. Based on the weighted optimal energy cost function and Schwarz inequality in different the heading angle segments, we obtain the general form of the optimal control command of the shaping guidance law and further design the cooperative shaping trajectory guidance law. The proposed guidance law can satisfy tactical requirements and restrictive conditions and it allows multiple cruise missiles cooperatively attack the target in different trajectories. The numeral simulation results demonstrate its effectiveness and advantages compared with proportion navigation guidance (PNG) algorithm.


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    Title :

    Cooperative Trajectory Shaping Guidance Law for Multiple Missiles


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Deng, Yimin (editor) / Yang, Guangyu (author) / Fang, YangWang (author) / Fu, Wenxing (author) / Wang, Zhikai (author) / Ma, Wenhui (author)

    Conference:

    International Conference on Guidance, Navigation and Control ; 2022 ; Harbin, China August 05, 2022 - August 07, 2022



    Publication date :

    2023-01-31


    Size :

    12 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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