A fault tolerant flight control system for sensor and actuator failures using neural networks

Marcello R. Napolitano, Younghwan An, Brad A. Seanor
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引用次数: 200

Abstract

In recent years neural networks have been proposed for identification and control of linear and non-linear dynamic systems. This paper describes the performance of a neural network-based fault-tolerant system within a flight control system. This fault-tolerant flight control system integrates sensor and actuator failure detection, identification, and accommodation (SFDIA and AFDIA). The first task is achieved by incorporating a main neural network (MNN) and a set of n decentralized neural networks (DNNs) to create a system with n sensors which has the ability to detect a wide variety of sensor failures. The second scheme implements the same main neural network integrated with three neural network controllers. The contribution of this paper focuses on enhancements of the SFDIA scheme to allow the handling of soft failures as well as addressing the issue of integrating the SFDIA and the AFDIA schemes without degradation of performance in terms of false alarm rates and incorrect failure identification. The results of the simulation with different actuator and sensor failures with a non-linear aircraft model are presented and discussed.

基于神经网络的传感器和执行器故障容错飞行控制系统
近年来,神经网络被提出用于线性和非线性动态系统的识别和控制。本文描述了飞行控制系统中基于神经网络的容错系统的性能。该容错飞行控制系统集成了传感器和执行器故障检测、识别和调节(SFDIA和AFDIA)。第一个任务是通过结合主神经网络(MNN)和一组n个分散神经网络(DNN)来创建一个具有n个传感器的系统来实现的,该系统能够检测各种传感器故障。第二种方案实现了与三个神经网络控制器集成的同一主神经网络。本文的贡献集中在增强SFDIA方案,以允许处理软故障,并解决在不降低误报率和错误故障识别性能的情况下集成SFDIA和AFDIA方案的问题。给出并讨论了非线性飞机模型在不同执行器和传感器故障情况下的仿真结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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