控制理论(社会学)
稳健性(进化)
运动学
制导系统
自适应控制
Lyapunov稳定性
计算机科学
路径(计算)
坐标系
李雅普诺夫函数
控制工程
工程类
控制(管理)
人工智能
非线性系统
航空航天工程
物理
基因
经典力学
化学
程序设计语言
量子力学
生物化学
作者
Kenan Yong,Mou Chen,Qingxian Wu
标识
DOI:10.1080/00207721.2019.1587544
摘要
An integrated guidance and control scheme is proposed on path following for the unmanned aerial vehicle. It is capable of handling the coupled non-linearities of the path's kinematics and the aircraft's dynamics independently. In the path coordinate, the guidance law is designed based on a nominal model, and the non-linearity of the path's kinematics is taken into full consideration. In the time coordinate, the flight control law is designed as a feed-forward controller, and it can guarantee the robustness of the guidance law with respect to the actual aircraft's dynamics. Instead of only employing Lyapunov method, the concept of immersion and invariance is also applied to explicitly analyse the stability in both time and path coordinates, and the asymptotic stability of the closed-loop system can be guaranteed. What is more, the regulation-based and immersion-based adaptive technologies are synthetically utilised to handle the unknown parameters. Finally, the numerical simulations demonstrate the effectiveness of the developed integrated guidance and control scheme.
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