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Observer based finite-time fault tolerant quadrotor attitude control with actuator faults

机译:基于Observer的有限时间容错耐动力态度控制与执行器故障

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摘要

This paper investigates a nonlinear robust fault tolerant control method for rejecting wind disturbances and accommodating actuator faults in quadrotor attitude system. Actuator faults are modeled as a sudden loss of actuator effectiveness (LAE) in the rotor thrust. First, the lumped disturbances, including wind disturbances and LAE actuator faults, are estimated by a novel adaptive finite-time extended state observer (AFTESO). Additionally, a rigorous analysis for finite-time convergence of estimation errors is provided. Next, based on the estimated information from AFTESO, a continuous fast nonsingular terminal sliding mode controller (CFNTSMC) is proposed to achieve high-precision tracking and finite-time convergence. CFNTSMC provides faster convergence performance in both reaching and sliding phases. The proposed control scheme combines ESO-based and NTSM-based anti-disturbance mechanisms, which retains the advantages of the two control schemes and limits their drawbacks, thus achieving promising features, as finite-time convergence, fault tolerance and chattering suppression. The finite-time stability of the closed-loop system is supported by Lyapunov theory. Finally, extensive numerical simulations are carried out to demonstrate the effectiveness of the proposed method in different working regimes. (C) 2020 Elsevier Masson SAS. All rights reserved.
机译:本文研究了拒绝风扰动和互动态度系统中的静电扰动和容纳致动器故障的非线性鲁棒容错控制方法。执行器故障在转子推力中被建模为突然丢失的致动器效果(LAE)。首先,通过新颖的自适应有限时间扩展状态观察器(AFTeso)估计包括风扰动和LAE执行器故障,包括风扰动和LAE执行器故障。另外,提供了对估计误差有限时间收敛的严格分析。接下来,基于来自AFTESO的估计信息,提出了一种连续的快速非垂直端子滑动模式控制器(CFNTSMC)以实现高精度跟踪和有限时间的收敛。 CFNTSMC在达到和滑动阶段提供更快的收敛性能。所提出的控制方案结合了基于ESO的和基于NTSM的抗扰度机制,其保留了两个控制方案的优点并限制了它们的缺点,从而实现了有前途的特征,作为有限时间收敛,容错和抖动抑制。 Lyapunov理论支持闭环系统的有限时间稳定性。最后,进行了广泛的数值模拟,以证明所提出的方法在不同的工作制度中的有效性。 (c)2020 Elsevier Masson SAS。版权所有。

著录项

  • 来源
    《Aerospace science and technology》 |2020年第9期|105968.1-105968.16|共16页
  • 作者单位

    Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Beijing Inst Technol Beijing Key Lab UAV Autonomous Control Beijing 100081 Peoples R China;

    Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Beijing Inst Technol Beijing Key Lab UAV Autonomous Control Beijing 100081 Peoples R China;

    Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Beijing Inst Technol Beijing Key Lab UAV Autonomous Control Beijing 100081 Peoples R China;

    Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Beijing Inst Technol Beijing Key Lab UAV Autonomous Control Beijing 100081 Peoples R China;

    Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Beijing Inst Technol Beijing Key Lab UAV Autonomous Control Beijing 100081 Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Quadrotor attitude control; Adaptive finite-time extended state observer (AFTESO); Continuous fast nonsingular terminal sliding mode control (CFNTSMC); Fault tolerant control; Lumped disturbances;

    机译:Quadrotor姿态控制;自适应有限时间扩展状态观察者(AFTESO);连续快速的非垂直端子滑动模式控制(CFNTSMC);容错控制;集失扰动;

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