Applications of Polynomial Neural Networks to FDIE and Reconfigurable Flight Control

R. Barron, R. L. Cellucci, P. Jordan, N. Beam, P. Hess, A. R. Barron
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引用次数: 10

Abstract

Fault detection, isolation, and estimation (FDIEI functions and reconfiguration strategres for Right control systems present major technical chaIImges, primarily because of uncertainties resulting from limited observability and an almost unlimited variety of malfunction and damage scenarios. This paper deals primarily with a portion of the probIem, i.e., global FDIE for single impairments of control effectors. Reference is also made to reconfiguration strategies. Polynomial neural networks are synthesized using a constrained error criterion to obtain pairwise discrimination between impaired and no-fail conditions and isolation h e e n impairment classes. The pairwise discrimi~tora~re thm combined in a form of voting logic Polynomial netwarks are also synthesized to obtain estimates of the amount af effector impairment. The Algorithm for Synthesis of Polynomial Networks (ASEN) arrd related methods are used to create the networks, which are highorder, linear or nonlinear, analytic, multivariate functions of the in-flight observables. This paper outlines the design procedure, including database preparation, extraction of waveform features, network synthesis techniques, and the architecture of the FDIE system that has been studied for the Control Reconfigurable Combat Aircraft. Representative performance results are prwvided.
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多项式神经网络在FDIE和可重构飞行控制中的应用
Right控制系统的故障检测、隔离和估计(FDIEI功能和重新配置策略)面临着主要的技术挑战,主要是因为有限的可观测性和几乎无限的故障和损坏场景所导致的不确定性。本文主要研究问题的一部分,即控制效应器单个损伤的全局FDIE问题。还参考了重新配置策略。利用约束误差准则合成多项式神经网络,实现损伤与非故障条件的两两区分和损伤类别间的隔离。将它们以投票逻辑多项式网络的形式组合在一起,合成了两两判别算子,以估计效应器损伤的量。利用多项式网络综合算法(ASEN)及相关方法,建立了飞行观测值的高阶、线性或非线性、解析、多元函数网络。本文概述了控制可重构作战飞机FDIE系统的设计过程,包括数据库的建立、波形特征的提取、网络合成技术以及FDIE系统的体系结构。给出了具有代表性的性能结果。
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