Cooperative guidance is a practical and challenging problem involving multiple coupling constraints, especially considering missile speed variation and target maneuvers. In this article, a wide-envelope cooperative guidance law is proposed for multiple speed-varying missiles with the field-of-view (FOV) constraint to simultaneously intercept a maneuvering target. First, the 3-D cooperative guidance problem is reformulated in a virtual coordinate frame to address the target maneuver. Next, a cooperative guidance law is developed based on the varying-gain proportional navigation guidance law, with an effective numerical algorithm predicting the time-to-go under time-varying speed. Then, the guidance law is modified by including a bias guidance term to satisfy the FOV constraint throughout the cooperative guidance. Since no linearized approximations are involved in the derivation, the resultant cooperative guidance law guarantees a wide launch envelope as well as high impact precision without actively adjusting missile speed. Extensive numerical simulations are performed to show the effectiveness of the suggested results.


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    Titel :

    Wide-Envelope Cooperative Guidance With Constrained Field-of-View and Varying Speed Against Maneuvering Targets


    Beteiligte:
    Yi, Xin (Autor:in) / Wang, Chunyan (Autor:in) / Dong, Wei (Autor:in) / Wang, Jianan (Autor:in) / Deng, Fang (Autor:in) / Xin, Ming (Autor:in)


    Erscheinungsdatum :

    01.08.2025


    Format / Umfang :

    11324738 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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