Considering the key characteristics of the aircraft only aiming at winning the pursuit-evasion (PE) game regardless of the effort when facing the incoming missiles, this paper studies the cooperative guidance problem of two air-to-air missiles attacking the same smart evading aircraft. It is assumed that both sides of the PE have the kinematic state parameters of each other, and then the “2vs1” problem is modeled in a modified differential game (DG) form using the line of sight (LOS) angular velocity as the state parameter. The min-max optimization expression is proposed by modifying the traditional cost function, and the state dependent Riccati equation (SDRE) method is used to derive the optimal controller of dual missiles and the escaping target. Finally, the simulation scenario is constructed to analyze and verify the performance of the proposed algorithm. Under the given simulation situations, the modified differential game cooperative guidance law is capable of cooperative attack tasks and the derived target evasion strategy is more in line with human experience.


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    Titel :

    Differential-Game Based Cooperative Guidance Law Against Maneuvering Target at All Costs


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Yan, Liang (Herausgeber:in) / Duan, Haibin (Herausgeber:in) / Yu, Xiang (Herausgeber:in) / Zhang, Jiaqiang (Autor:in) / Li, Wangxi (Autor:in) / Qi, Duo (Autor:in) / Liang, Xiaolong (Autor:in) / Ren, Baoxiang (Autor:in)


    Erscheinungsdatum :

    2021-10-30


    Format / Umfang :

    11 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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