Research on Target State Estimation and Terminal Guidance Algorithm in the Process of Multi-UAV Cooperative Attack

Tang, Zhongnan; Wang, Yujie; Chen, Qingyang; Yang, X. H.

doi:10.1109/cacre50138.2020.9229963

Cited by 3 publications

(1 citation statement)

References 4 publications

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“…Krizmancic et al [ 28 ] designed the optimal guidance and control method to meet the missile terminal constraints by reasonably optimizing the allocation of acceleration commands in the guidance system based on the landing angle constraints and acceleration constraints. Tang et al [ 29 ] first established an offset proportional guidance law for a single missile and finally formed a networked cooperative guidance and control method with landing angle and time constraints by adjusting the remaining attack time of other missiles in real time. Li and Ma [ 30 ] designed an optimal controller suitable for multimissile cooperative attack based on the idea of lead missile and slave missile.…”

Section: Swarm Guidance and Control Of The Missilementioning

confidence: 99%

Intelligent Guidance and Control Methods for Missile Swarm

Huang

Zhao

Zhang

2022

Computational Intelligence and Neuroscience

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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.

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Section: Swarm Guidance and Control Of The Missilementioning

confidence: 99%