Robust Intelligent Guidance Law for Missile Interception Based on Prescribed Performance

被引：0
|
作者：
Yan T. [1 ]
Cheng H. [1 ]
Gao M. [1 ]
Guo Y. [2 ]
Xu B. [3 ]
机构：
[1] Unmanned System Research Institute, Northwestern Polytechnical University, Xi'an
[2] School of Automation Science and Engineering, South China University of Technology, Guangzhou
[3] School of Automation, Northwestern Polytechnical University, Xi'an
来源：
Yuhang Xuebao/Journal of Astronautics | 2024年 / 45卷 / 05期
关键词：
Composite learning; Integrated guidance and control; Missile interception; Model uncertainty; Prescribed performance control;
D O I：
10.3873/j.issn.1000-1328.2024.05.010
中图分类号：
学科分类号：
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. © 2024 Chinese Society of Astronautics. All rights reserved.
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页码：753 / 761
页数：8
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