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Fault-tolerant control for a quadrotor unmanned helicopter subject to sensor faults

机译:具有传感器故障的四旋翼无人直升机的容错控制

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This paper presents an active fault-tolerant control scheme for a quadrotor unmanned helicopter with velocity sensor faults. A two-level control scheme is designed to guarantee the trajectory following of the quadrotor when there are no faults. The control scheme consists of an external-loop Proportion Differentiation (PD) control law and an internal-loop Proportion Integration Differentiation (PID) control law. A fault diagnosis unit is designed to detect and estimate sensor faults. The fault detection is achieved by using an observer-based residual generator of a Luenberger type and the fault estimation problem is solved by utilizing an augment variable observer. The asymptotical convergence property of estimation errors is proved. A fault-tolerant control law is proposed by combing the external-loop PD control law and the result of fault estimation. Finally, the experimental results demonstrate the effectiveness of the scheme.
机译:本文提出了一种具有速度传感器故障的四旋翼无人直升机的主动容错控制方案。设计了两级控制方案,以确保在无故障时四旋翼的轨迹跟随。该控制方案包括一个外环比例微分(PD)控制律和一个内环比例微分(PID)控制律。故障诊断单元设计用于检测和估计传感器故障。通过使用基于观察者的Luenberger类型的残差生成器来实现故障检测,并通过使用增量变量观察器来解决故障估计问题。证明了估计误差的渐近收敛性。通过结合外环PD控制律和故障估计结果,提出了一种容错控制律。最后,实验结果证明了该方案的有效性。

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