摘要
We present two different methods of reaction control system (RCS) jet selection logic (JSL) reconfiguration; (1) assembled logic searching, (2) linear programming based on impulse moment control. In the full paper, we explain in some detail our two methods of JSL reconfiguration; in this abstract, we just add some pertinent remarks to listing the two topics of explanation. The first topic is: the method of JSL reconfiguration based on assembled logic searching. In the first topic, after explaining the principles of JSL reconfiguration, we give three specific steps of JSL reconfiguration. The second topic is: the linear programming method of JSL reconfiguration based on impulse moment control. In the second topic, we first explain the principles of linear programming method and then discuss its pros and cons as compared with the JSL reconfiguration method based on assembled logic searching. Finally, using the back RCS schematic of American X-34 technology demonstrator, we performed simulations, whose results are given in Figs. 2 through 9 in the full paper. These results show preliminarily that the two different methods proposed by us are both effective; when RCS jet fails to fire, although the control performance deteriorates quite considerably, such deterioration is still allowable.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 794-799 |
| 页数 | 6 |
| 期刊 | Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University |
| 卷 | 25 |
| 期 | 6 |
| 出版状态 | 已出版 - 12月 2007 |
指纹
探究 'Two different methods of JSL reconfiguration for reusable launch vehicle's reentry phase' 的科研主题。它们共同构成独一无二的指纹。引用此
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