反推
控制理论(社会学)
非线性系统
沉降时间
Lyapunov稳定性
自适应控制
欧拉角
计算机科学
常量(计算机编程)
李雅普诺夫函数
跟踪(教育)
控制器(灌溉)
控制(管理)
数学
控制工程
工程类
人工智能
心理学
教育学
农学
物理
几何学
量子力学
生物
阶跃响应
程序设计语言
作者
Vijay Kumar Singh,Shyam Kamal
出处
期刊:IEEE Transactions on Circuits and Systems Ii-express Briefs
[Institute of Electrical and Electronics Engineers]
日期:2023-04-18
卷期号:70 (11): 4138-4142
被引量:7
标识
DOI:10.1109/tcsii.2023.3267944
摘要
This brief addresses the prescribed-time attitude tracking issue for an uncertain nonlinear 2-Degree of Freedom (DOF) helicopter. Based on the Euler-Lagrange equations, a nonlinear model is developed for the 2-DOF helicopter, where the system parameters and control input constant coefficients are unknown. The proposed prescribed-time control is based on adaptive backstepping and utilized to track the desired pitch and yaw positions separately. Using the theory of Lyapunov stability, we show that the proposed prescribed-time control and adaptive law ensure the boundedness of all the closed-loop signals of the system for all future time. A noticeable advantage of the proposed method is that the upper bound of the settling time can be specified in advance. Finally, to verify the efficacy and control capabilities of the proposed scheme, simulations are conducted on the Quanser 2-DOF helicopter system.
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