首页> 外文会议>International Conference on Unmanned Aircraft Systems >Fault-tolerant control for a quadrotor unmanned helicopter subject to sensor faults
【24h】

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

机译:用于传感器故障的四轮压力机无人直升机的容错控制

获取原文

摘要

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轮电机无人直升机的积极容错控制方案。旨在保证两级控制方案,以保证在没有故障时按Quadrotor的轨迹。控制方案包括外环比例分化(PD)控制法和内环比例集成分化(PID)控制定律。故障诊断单元旨在检测和估计传感器故障。通过使用Luenberger类型的基于观察者的剩余发生器来实现故障检测,并且通过使用增强可变观察者来解决故障估计问题。证明了估计误差的渐近收敛性。通过梳理外环PD控制法以及故障估计结果来提出容错控制定律。最后,实验结果表明了该方案的有效性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号