Stress-deflection angle measurement of the aircraft wings using a biaxial inclination angle sensor
文献类型：会议论文
| 作者 | Tian, Peng; Li, Fan-xing; Yin, Gui-gang; Wang, Da-kui; Hu, Song; Yan, Wei |
| 出版日期 | 2018 |
| 会议日期 | JUL 06-08, 2018JUL 06-08, 2018 |
| 会议地点 | Xiamen, PEOPLES R CHINAXiamen, PEOPLES R CHINA |
| 关键词 | space rotation shaft biaxial inclination angle sensor space coordinate transformation |
| DOI | 10.1109/FENDT.2018.8681983 |
| 页码 | 18-21 |
| 英文摘要 | The flight pose of an aircraft is affected seriously by the stress-deflection angles of aileron and tail fin. Traditional manual measurement suffers from various error sources. Here, we propose a novel high precision measuring method. A biaxial inclination angle sensor is used to calculate the unit-normal-vector of the measuring plane. Levelling is the first and necessary step to make zero for X and Y axes. Those values of the two axes are eliminated by the space coordinate transformation between rotation shaft and rotary surface, meanwhile, the changing value of Z axis is utilized to figure out the space stress-deflection angle. The proof of -concept experiments verify that the improved automation and precision can be achieved by the proposed technique. Furthermore, the measurement is not constrained by the shape of the curved surface of the object. Those advantages make the method suitable in space deflection angle measurement of giant space rotation structure, especially in aerospace field. |
| 会议录 | PROCEEDINGS OF 2018 IEEE FAR EAST NDT NEW TECHNOLOGY & APPLICATION FORUM (IEEE FENDT 2018)
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| 文献子类 | C |
| 语种 | 英语 |
| WOS记录号 | WOS:000468889700004 |
| 源URL | [http://ir.ioe.ac.cn/handle/181551/9126]  |
| 专题 | 光电技术研究所_微电子装备总体研究室（四室） |
| 推荐引用方式 GB/T 7714 | Tian, Peng,Li, Fan-xing,Yin, Gui-gang,et al. Stress-deflection angle measurement of the aircraft wings using a biaxial inclination angle sensor[C]. 见:. Xiamen, PEOPLES R CHINAXiamen, PEOPLES R CHINA. JUL 06-08, 2018JUL 06-08, 2018. |
入库方式： OAI收割
来源：光电技术研究所
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