In order to improve the penetration and strike capability of unmanned aerial vehicles (UAVs), a cooperative guidance law is presented for multiple UAVs attacks on the same maneuvering target. Firstly, based on the finite-time consistency convergence theory, a multiple UAVs time cooperative guidance law is designed, the guidance law is not bound by the end time, which enhances the anti-interference ability during the guidance period. Secondly, based on the sliding mode variable structure control theory, the guidance law of multiple UAVs attack angle constraint is designed; the guidance law is optimized according to the quasi- sliding mode control, which weakens the chattering of the sliding mode. Finally, the simulation verifies the effectiveness of the designed guidance law.


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    Titel :

    Time-Cooperative Guidance Law for Multiple UAVs with Angle Constraints


    Beteiligte:
    Yi, Zhang (Autor:in) / Guowei, Fang (Autor:in) / Xiuxia, Yang (Autor:in) / Weiyi, Cao (Autor:in) / Xuan, Yan (Autor:in)


    Erscheinungsdatum :

    01.10.2019


    Format / Umfang :

    2961439 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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