This paper proposes a three-dimensional prescribed performance cooperative guidance laws for intercepting maneuvering targets. The laws can ensure that multiple missiles to simultaneously intercept a maneuvering target with space constraints. The relative distance between multiple missiles and target are chosen as a coordination variable to avoid the estimation error caused by the inaccurate time-to-go. A new error transformed function (ETF) and sliding mode surface are proposed, and the boundedness of tanh function is utilized to ensure the prescribed performance of the line-of-sight (LOS) angle. An adaptive law is proposed to deal with the unknown maneuvering information of the target. The simulation results are presented to demonstrated the effectiveness of the proposed guidance law.


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    Title :

    Three-Dimensional Prescribed Performance Space-Time Cooperative Guidance Law for Intercepting Maneuvering Target


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Ren, Zhang (editor) / Wang, Mengyi (editor) / Hua, Yongzhao (editor) / Ma, Meng-chen (author) / Song, Shen-min (author) / Liu, Bin (author)


    Publication date :

    2022-07-29


    Size :

    11 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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