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Adaptive finite-time fault-tolerant formation control for quadrotors with actuator faults

机译:具有执行器故障的四旋翼的自适应有限时容错编队控制

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In this paper, the finite-time formation control of a group of quadrotor aircrafts with a leader is studied. Using adaptive update mechanism and boundary layer theory, a continuous finite-time fault-tolerant formation control protocol is constructed to compensate for actuator faults. The results show that using the proposed fault-tolerant controller can achieve the desired pattern of formation and the desired trajectory under actuator faults. Finally, a simulation example is given to show the effectiveness of the proposed method.
机译:本文研究了一组带引导的四旋翼飞机的有限时间编队控制。利用自适应更新机制和边界层理论,构造了一种连续的有限时间容错编队控制协议来补偿执行器故障。结果表明,使用所提出的容错控制器可以在致动器故障下实现所需的形成模式和所需的轨迹。最后,通过仿真实例说明了该方法的有效性。

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