With the complexity of the modern battlefield environment and the diversification of combat missions, the performance of weapons and equipment continues to improve. In the increasingly fierce offensive and defensive confrontation, the difficulty of a single missile to penetrate the defense has increased significantly, and the mode of multi-missile group cooperative combat has become today’s research. The multi-projectile cooperative guidance technology is the key technology. This paper first analyzes the constraint conditions in the cooperative terminal guidance of multiple missiles. Secondly, based on the establishment of the relative motion equations of the multiple missiles and targets, a multi-missile cooperative terminal guidance algorithm is proposed based on the bias proportional guidance law. Under the constraint that the missile meets the expected terminal attack angle, all missiles can hit the target at the same time. Finally, simulations verify the effectiveness of the proposed collaborative guidance algorithm.


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    Title :

    Design of Multi-constraints Missiles Cooperative Terminal Guidance Algorithm


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Wu, Meiping (editor) / Niu, Yifeng (editor) / Gu, Mancang (editor) / Cheng, Jin (editor) / Wan, Jiaqing (author) / Wang, Jian (author) / Guo, Qiang (author) / Li, Xinguo (author)

    Conference:

    International Conference on Autonomous Unmanned Systems ; 2021 ; Changsha, China September 24, 2021 - September 26, 2021



    Publication date :

    2022-03-18


    Size :

    15 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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