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作动器故障下的无人机容错控制方法
引用本文:崔玉伟,孙雪.作动器故障下的无人机容错控制方法[J].海军航空工程学院学报,2023,38(6):449-456.
作者姓名:崔玉伟  孙雪
作者单位:航空工业西安飞行自动控制研究所飞行控制系统部,陕西西安 710000 ;飞行控制航空科技重点实验室,陕西西安 710065
摘    要:在执行任务过程中,无人机的传感器、作动器等均可能出现故障。文章针对常规布局无人机的作动器故障,提出了 1种反步法和控制分配相结合的容错控制方法。首先,建立无人机数学模型,并对作动器故障进行分类和建模;然后,根据模型设计反步最优控制器和基于控制分配的容错控制器;最后,通过仿真验证表明,所设计的容错控制方法能够实现作动器故障下的姿态快速稳定控制,且稳定性好,基本无侧滑角,各操纵面均在约束范围内,达到容错控制要求。

关 键 词:作动器故障  反步法  控制分配  容错控制

Fault-Tolerant Control Method of UAV Under Actuator Fault
CUI Yuwei,SUN Xue.Fault-Tolerant Control Method of UAV Under Actuator Fault[J].Journal of Naval Aeronautical Engineering Institute,2023,38(6):449-456.
Authors:CUI Yuwei  SUN Xue
Abstract:In the course of UAV flight, the sensors and actuators of the UAV may fail. A fault-tolerant control method combining reverse step method and control distribution is proposed to solve the actuator fault of conventional layout UAV. Firstly, the UAV mathematical model is established, and the actuator fault is classified and modeled. Secondly, the reverse step optimal controller and fault-tolerant controller based on control assignment are designed according to the model. Finally, through simulation verification, the experimental results show that the designed fault tolerant control meth-od can realize the fast and stable attitude control under the fault of the actuator, and the stability is good, basically no side-slip angle, and each control surface is within the constraint range, meeting the fault tolerant control requirements.
Keywords:actuator fault  backstep method  control allocation  fault-tolerant control
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