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Cooperative guidance law based on super-twisting observer for target maneuvering

  • Mengjing Gao
  • , Tian Yan
  • , Bingjie Han
  • , Haoyu Cheng
  • , Wenxing Fu
  • , Bo Han
  • Northwestern Polytechnical University Xian
  • Aeronautic Computing Technique Research Institute
  • 93525 Troops

科研成果: 期刊稿件文章同行评审

6 引用 (Scopus)

摘要

To solve the problem that multiple missiles should simultaneously attack unmeasurable maneuvering targets, a guidance law with temporal consistency constraint based on the super-twisting observer is proposed. Firstly, the relative motion equations between multiple missiles and targets are established, and the topological model among multiple agents is considered. Secondly, based on the temporal consistency constraint, a cooperative guidance law for simultaneous arrival with finite-time convergence is derived. Finally, the unknown target maneuvering is regarded as bounded interference. Based on the second-order sliding mode theory, a super-twisting sliding mode observer is devised to observe and track the bounded interference, and the stability of the observer is proved. Compared with the existing research, this approach only needs to obtain the sliding mode variable which simplifies the design process. The simulation results show that the designed cooperative guidance law for maneuvering targets achieves the expected effect. It ensures successful cooperative attacks, even when confronted with strong maneuvering targets.

源语言英语
页(从-至)1304-1314
页数11
期刊Journal of Systems Engineering and Electronics
35
5
DOI
出版状态已出版 - 10月 2024

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