基于预设性能的导弹拦截鲁棒智能制导律

Tian Yan, Haoyu Cheng, Mengjing Gao, Yuyan Guo, Bin Xu

科研成果: 期刊稿件文章同行评审

摘要

Aiming at the missile interception problem with model uncertainty,a composite learning method combined with prescribed performance control is studied. Firstly,an integrated guidance and control model for missile interception is constructed. To ensure the constraint on the miss distance between the two sides,the prescribed performance function is utilized to guarantee the tracking performance. To improve the system accuracy against the model uncertainty,a composite learning law is constructed to estimate the unknown nonlinear functions of the system online. Finally,through Lyapunov analysis,the system stability is proved. Simulation results show that the proposed algorithm can successfully intercept the target and keep the tracking error within the specified performance curve,which demonstrates the effectiveness of the algorithm.

投稿的翻译标题Robust Intelligent Guidance Law for Missile Interception Based on Prescribed Performance
源语言繁体中文
页(从-至)753-761
页数9
期刊Yuhang Xuebao/Journal of Astronautics
45
5
DOI
出版状态已出版 - 5月 2024

关键词

  • Composite learning
  • Integrated guidance and control
  • Missile interception
  • Model uncertainty
  • Prescribed performance control

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