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首页> 外文期刊>Transactions of the Institute of Measurement and Control >Robust attitude fault-tolerant control for unmanned autonomous helicopter with flapping dynamics and actuator faults
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Robust attitude fault-tolerant control for unmanned autonomous helicopter with flapping dynamics and actuator faults

机译:振动动力学和执行器故障的无人自主直升机的鲁棒态度容错控制

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摘要

In this paper, an adaptive robust fault-tolerant control scheme is developed for attitude tracking control of a medium-scale unmanned autonomous helicopter with rotor flapping dynamics, external unknown disturbances and actuator faults. For the convenience of control design, the actuator dynamics with respect to the tail rotor are introduced. The adaptive fault observer and robust item are employed to observe the actuator faults and eliminate the effect of external disturbances, respectively. A backstepping-based robust fault-tolerant control scheme is designed with the aim of obtaining satisfactory tracking performance and closed-loop system stability is proved via Lyapunov analysis, which guarantees the convergence of all closed-loop system signals. Simulation results are given to show the effectiveness of the proposed control method.
机译:在本文中,开发了一种自适应稳健的容错控制方案,用于带有转子拍打动态的中型无人自主直升机的姿态跟踪控制,外部未知干扰和执行器故障。 为了便于控制设计,引入了相对于尾转子的致动器动力学。 采用自适应故障观察者和强大的项目来观察致动器故障并分别消除外部干扰的影响。 基于BackStepping的鲁棒容错控制方案旨在获得令人满意的跟踪性能,并通过Lyapunov分析证明闭环系统稳定性,可确保所有闭环系统信号的收敛性。 给出了仿真结果表明所提出的控制方法的有效性。

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