Multiple-fault diagnosis for spacecraft attitude control systems using RBFNN-based observers

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초록

In this paper, a novel multiple-fault diagnosis (MFD) scheme using radial basis function neural network (RBFNN)-based observers is presented for a spacecraft attitude control system (ACS) in the presence of external disturbances and nonlinear uncertainties. Based on dynamic and kinematic models, robust fault detection observers (FDOs) are designed to detect the simultaneous occurrence of actuator, gyro, and star sensor faults. Then, a series of RBFNN-based fault isolation observers (FIOs) are designed to decouple the faults of different components completely. This complete decoupling will guarantee that the diagnosis result of one component is not affected by the faults of other components; thus, multiple faults can be diagnosed simultaneously. To improve the accuracy of fault detection and reconstruction, disturbance compensation observers (DCOs) based on the RBFNN are also designed to compensate for the external disturbances. It is worth noting that the developed fault diagnosis scheme can be used to detect and isolate small faults. Finally, simulation results are presented to show the effectiveness and feasibility of the proposed method. (C) 2020 Elsevier Masson SAS. All rights reserved.

키워드

Multiple-fault diagnosis (MFD)Fault isolation observer (FIO)Disturbance compensation observer (DCO)Small fault detectionAttitude control system (ACS)NONLINEAR-SYSTEMSSENSORSATELLITEACTUATORGYROSCOPESSCHEME
제목
Multiple-fault diagnosis for spacecraft attitude control systems using RBFNN-based observers
저자
Guo, Xiang-GuiTian, Meng-EnLi, QingAhn, Choon KiYang, Yan-Hua
DOI
10.1016/j.ast.2020.106195
발행일
2020-11
유형
Article
저널명
Aerospace Science and Technology
106