控制理论(社会学)
弹道
趋同(经济学)
计算机科学
滑模控制
李雅普诺夫函数
控制器(灌溉)
带宽(计算)
跟踪(教育)
理论(学习稳定性)
控制工程
Lyapunov稳定性
模式(计算机接口)
转化(遗传学)
控制系统
车辆动力学
工程类
方向(向量空间)
国家(计算机科学)
功能(生物学)
边界(拓扑)
指数稳定性
跟踪误差
跟踪系统
稳健性(进化)
角速度
控制(管理)
作者
Lanfeng Hua,Wenhao Wang,Kaibo Shi,Jin Yang,Qishui Zhong,Hongjing Liang
标识
DOI:10.1109/tce.2025.3650623
摘要
This paper proposes a safety-critical fixed-time sliding mode control (SMC) strategy for quadrotor unmanned aerial vehicles (UAVs) to achieve precise trajectory tracking under external disturbances and prescribed performance constraints. A fixed-time prescribed performance function is first introduced, and by incorporating the state transformation technique into the SMC design, the proposed method guarantees that the closed-loop systems converge to prescribed small neighborhoods of zero within fixed time. Simultaneously, the tracking errors are strictly confined within user-defined safety boundaries at all times, despite external disturbances. To mitigate communication bandwidth limitations, a dynamic event-triggered mechanism is further developed for electronic speed-data transmission. Fixed-time convergence to the sliding surfaces and overall system stability are rigorously established using Lyapunov stability theory. Moreover, a cascaded control architecture is devised, wherein the proposed controller determines the desired accelerations, which are then utilized to compute the corresponding orientation and angular rates. Compared with existing tracking control approaches, the proposed framework not only ensures rapid convergence and guaranteed tracking performance but also significantly reduces communication overhead. The effectiveness and advantages of the method are demonstrated through simulation results.
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