牵引
弹道
非线性系统
控制理论(社会学)
跟踪(教育)
航空航天工程
控制(管理)
计算机科学
环境科学
控制工程
航空学
海洋工程
工程类
物理
人工智能
教育学
量子力学
心理学
天文
作者
Yuxin Cui,Z H Yao,Zhang Hong-yan,Tao Ni,Chaofei Wang
出处
期刊:Journal of physics
[IOP Publishing]
日期:2024-11-01
卷期号:2882 (1): 012054-012054
标识
DOI:10.1088/1742-6596/2882/1/012054
摘要
Abstract In this paper, for the towing problem of wheeled aircraft, an automatic control method is proposed based on the nonlinear control theory, which realizes the trajectory tracking of the aircraft by controlling the velocity of the towing point of the aircraft, so as to realize the aircraft’s outbound and inbound operations. Firstly, based on the nonholonomic constraint theory, the mathematical model of the aircraft towing system is established, and the kinematic relationship between the aircraft towing point and the aircraft is obtained. Then, a controller is designed based on the nonlinear control theory, and the stability analysis is carried out using the Lyapunov method to realize the trajectory tracking of the aircraft traction system. Finally, the effectiveness and accuracy of the control method are verified by the combination of MATLAB simulation analysis and scaled-down model experiment. The results show that the proposed control method can realize the trajectory control of the aircraft towing system.
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