摘要
Because of the special characteristics of spacecraft attitude control system that its precision model is not available and the knowledge-based method is not effective for it, adopting qualitative/quantitative hybrid fault diagnosis and combining the case-based reasoning method with parity space, the qualitative/quantitative hybrid fault diagnosis method based on case-based reasoning and parity space is proposed in this paper. The method is based on building a qualitative/quantitative hybrid fault diagnosis model. The spacecraft attitude control system is taken as an illustrative example, and the result shows that the proposed qualitative/quantitative hybrid fault diagnosis method is more effective than each individual method.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 87-90 |
| 页数 | 4 |
| 期刊 | Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics |
| 卷 | 43 |
| 期 | SUPPL.1 |
| 出版状态 | 已出版 - 7月 2011 |
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