首页> 外文学位 >Dynamic neural network-based Pulsed Plasma Thruster (PPT) fault detection and isolation for the Attitude Control Subsystem of formation flying satellites.
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Dynamic neural network-based Pulsed Plasma Thruster (PPT) fault detection and isolation for the Attitude Control Subsystem of formation flying satellites.

机译:基于动态神经网络的脉冲等离子推进器(PPT)故障检测和隔离,用于编队飞行卫星的姿态控制子系统。

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摘要

The main objective of this thesis is to develop a dynamic neural network-based fault detection and isolation (FDI) scheme for the Pulsed Plasma Thrusters (PPTs) that are used in the Attitude Control Subsystem (ACS) of satellites that are tasked to perform a formation flying mission. In order to accomplish these objectives three fault detection and isolation (FDI) approaches based on dynamic neural networks (DNN) are developed: (i) a "Low Level" FDI scheme, (ii) a "High Level" FDI scheme, and (iii) an "Integrated" FDI scheme. Based on data that is collected from the electrical circuit of the PPTs, our proposed "Low Level" FDI scheme can detect and isolate faults in the PPT actuators. Using a Confusion Matrix evaluation system we demonstrate that can achieve a high level of accuracy but the precision level is below expectations and the misclassification rate is expressed as False Healthy and False Faulty parameters is significant. Our proposed "High Level" FDI scheme utilizes data collected from the relative attitudes of the formation flying satellites. According to the simulation results, our proposed FDI scheme can detect the pair of thrusters which is faulty. It represents a promising detection capability, however its isolation capabilities are not adequate. Finally, our proposed "Integrated" FDI scheme takes advantage of the strengths of each of the previous schemes and at same time reduces their individual weaknesses. To demonstrate its capabilities, various fault scenarios were simulated. The results demonstrate a high level of accuracy (99.79%) and precision (99.94%) with a misclassification rate that is quite negligible. Furthermore, our proposed "Integrated" FDI scheme provides additional and interesting information related to the effects of faults in the thrust production levels that would not be available from simply the low and high levels separately.
机译:本论文的主要目的是为脉冲姿态推进器(PPT)开发一种基于动态神经网络的故障检测和隔离(FDI)方案,该方案用于执行任务的卫星姿态控制子系统(ACS)中。编队飞行任务。为了实现这些目标,开发了基于动态神经网络(DNN)的三种故障检测和隔离(FDI)方法:(i)一种“低级” FDI方案,(ii)一种“高级” FDI方案,以及( iii)“综合”外国直接投资计划。基于从PPT电路收集的数据,我们提出的“低水平” FDI方案可以检测并隔离PPT执行器中的故障。使用混淆矩阵评估系统,我们证明可以达到较高的准确度,但准确度低于预期,并且误分类率表示为False Healthy和False Fault参数很重要。我们提出的“高级” FDI计划利用从编队飞行卫星的相对姿态收集的数据。根据仿真结果,我们提出的FDI方案可以检测出故障的一对推进器。它代表了有前途的检测能力,但是其隔离能力却不足。最后,我们提出的“集成” FDI计划利用了每个先前计划的优势,同时减少了它们各自的弱点。为了演示其功能,模拟了各种故障情况。结果显示出较高的准确度(99.79%)和精密度(99.94%),并且错误分类率可以忽略不计。此外,我们提出的“集成” FDI方案提供了与推力生产水平中的断层影响有关的其他有趣信息,而这些信息不能仅从低水平和高水平单独获得。

著录项

  • 作者

    Valdes, Arturo.;

  • 作者单位

    Concordia University (Canada).;

  • 授予单位 Concordia University (Canada).;
  • 学科 Engineering Electronics and Electrical.
  • 学位 M.A.Sc.
  • 年度 2008
  • 页码 145 p.
  • 总页数 145
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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