Adaptive sensor fault tolerant control with prescribed performance for unmanned autonomous helicopter based on neural networks

IF 1.2 4区 工程技术 Q3 ENGINEERING, AEROSPACE
Min Wan, Mou Chen, Mihai Lungu
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引用次数: 0

Abstract

Purpose

This paper aims to study a neural network-based fault-tolerant controller to improve the tracking control performance of an unmanned autonomous helicopter with system uncertainty, external disturbances and sensor faults, using the prescribed performance method.

Design/methodology/approach

To ensure that the tracking error satisfies the prescribed performance, the authors adopt an error transformation function method. A control scheme based on the neural network and high-order disturbance observer is designed to guarantee the boundedness of the closed-loop system. A simulation is performed to prove the validity of the control scheme.

Findings

The developed adaptive fault-tolerant control method makes the system with sensor fault realize tracking control. The error transformation function method can effectively handle the prescribed performance requirements. Sensor fault can be regarded as a type of system uncertainty. The uncertainty can be approximated accurately using neural networks. A high-order disturbance observer can effectively suppress compound disturbances.

Originality/value

The tracking performance requirements of unmanned autonomous helicopter system are considered in the design of sensor fault-tolerant control. The inequality constraint that the output tracking error must satisfy is transformed into an unconstrained problem by introducing an error transformation function. The fault state of the velocity sensor is considered as the system uncertainty, and a neural network is used to approach the total uncertainty. Neural network estimation errors and external disturbances are treated as compound disturbances, and a high-order disturbance observer is constructed to compensate for them.

基于神经网络的无人自主直升机自适应传感器容错控制与规定性能
目的 本文旨在研究一种基于神经网络的容错控制器,利用规定性能法改善具有系统不确定性、外部干扰和传感器故障的无人自主直升机的跟踪控制性能。设计了一种基于神经网络和高阶干扰观测器的控制方案,以保证闭环系统的有界性。研究结果所开发的自适应容错控制方法使带有传感器故障的系统实现了跟踪控制。误差变换函数方法能有效地满足规定的性能要求。传感器故障可视为系统不确定性的一种。利用神经网络可以对不确定性进行精确近似。高阶扰动观测器能有效抑制复合扰动。原创性/价值在设计传感器容错控制时考虑了无人自主直升机系统的跟踪性能要求。通过引入误差变换函数,将输出跟踪误差必须满足的不等式约束转化为无约束问题。速度传感器的故障状态被视为系统的不确定性,使用神经网络来接近总的不确定性。神经网络估计误差和外部干扰被视为复合干扰,并构建了一个高阶干扰观测器对其进行补偿。
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来源期刊
Aircraft Engineering and Aerospace Technology
Aircraft Engineering and Aerospace Technology 工程技术-工程:宇航
CiteScore
3.20
自引率
13.30%
发文量
168
审稿时长
8 months
期刊介绍: Aircraft Engineering and Aerospace Technology provides a broad coverage of the materials and techniques employed in the aircraft and aerospace industry. Its international perspectives allow readers to keep up to date with current thinking and developments in critical areas such as coping with increasingly overcrowded airways, the development of new materials, recent breakthroughs in navigation technology - and more.
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