High-speed unmanned aerial vehicles (UAVs) are more and more widely used in both military and civil fields at present, especially the missile swarm attack, and will play an irreplaceable key role in the future war as a special combat mode. This study summarizes the guidance and control methods of missile swarm attack operation. First, the traditional design ideas of the guidance and control system are introduced; then, the typical swarm attack guidance and control methods are analyzed by taking their respective characteristics into considering, and the limitations of the traditional design methods are given. On this basis, the study focuses on the advantages of intelligent integrated guidance and control design over traditional design ideas, summarizes the commonly used integrated guidance and control design methods and their applications, and explores the cooperative attack strategy of missile swarm suitable for the integrated guidance and control system. Finally, the challenges of missile swarm guidance and control are described, and the problems worthy of further research in the future are prospected. Summarizing the guidance and control methods of missile will contribute to the innovative research in this field, so as to promote the rapid development of unmanned swarm attack technology.


    Access

    Download


    Export, share and cite



    Title :

    Intelligent Guidance and Control Methods for Missile Swarm


    Contributors:
    Hanqiao Huang (author) / Xin Zhao (author) / Xiaoyan Zhang (author)


    Publication date :

    2022




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




    Missile Guidance Algorithm Design Using Particle Swarm Optimization

    Kung, Chien-Chun / Chen, Kuei-Yi | Tema Archive | 2013



    Missile Guidance and Control Systems

    Siouris, George M. | TIBKAT | 2004


    Missile guidance and control systems

    Siouris, George M. | TIBKAT | 2004


    Advanced missile guidance

    LAWRENCE, R. | AIAA | 1991