期刊文献+

飞机结构件运动数据的动态视觉测量系统 被引量:13

Optical and dynamic measuring system for movement data of aircraft structural parts
下载PDF
导出
摘要 基于近景摄影测量理论和立体视觉技术,提出并实现了一种针对机身结构件在飞行状态下的轨迹、姿态、位移、变形等多种运动数据的动态视觉测量方法。研究了基于工业近景摄影测量的多相机快速自标定方法;飞行状态下相机动态定位及抖动消除技术;刚性结构件的运动轨迹及姿态的快速求取和通过多相机(≥3)协作实现非编码标志点阵列的精确匹配等多项关键技术。在模拟飞行环境下的实验结果表明,相机标定的重投影误差小于0.03pixel,系统的运动轨迹姿态测量精度可达0.01mm/1m,关键点位移变形测量精度可达0.05mm/1m,基本满足飞机测试行业的精度和可靠性测量标准。 In order to obtain the movement data of an aircraft, including trajectory, attitude, displace- ment, deformation and other kinds of movement data of the aircraft structural parts in the flight accu- rately, an optical and dynamic measurement method is proposed and implemented based on the theory of close-range photogrammetry and stereo vision technology. The main contents of the method are multi-camera self-calibration technique based on close-range photogrammetry, camera dynamic posi- tioning and jitter eliminating in flight technology, rapid acquisition for the trajectory and attitude of rigid structure, precise matching of non-coding landmark array by multi-camera (≥3) collaboration. The simulation results show that the reprojection error of the camera is less than 0.03 pixel, the traj- ectory and attitude measurement accuracy of the system can be up to 0.01 mm/1 m, and the measure- ment accuracy of key point displacement and deformation is 0.05 ram/1 m. It demonstrates that the system have met the standards of accuracy and reliability for aircraft testing industry.
出处 《光学精密工程》 EI CAS CSCD 北大核心 2012年第9期1929-1938,共10页 Optics and Precision Engineering
基金 国家科学自然基金资助项目(No.50975219) 江苏省科技支撑计划资助项目(No.BE2008058)
关键词 相机自标定 相机动态定位 轨迹姿态求取 多相机匹配 立体视觉 camera self-calibration camera dynamic positioning trajectory and attitude acquisition multi-camera matching stereo vision
  • 相关文献

参考文献16

  • 1BURNER A W, LIU T SH. Videogrammetric model deformation measurement technique[J].Journal of Aircraft, 2001, 38 (4): 745-754. 被引量:1
  • 2BLACK J T, PITCHER N A, aREEDER M F, et al: Videogrammetry dynamics measurements of a lightweight flexible wing in a wind tunnel[J]. Journal of Aircraft, 2010, 47 (1): 172-180. 被引量:1
  • 3BURNER A W, LOKOS W A, BARROWS D A. Aero- elastic deformation: adaptation of wind tunnel measure- ment concepts to full-scale vehicle flight testing[C]. Symposium on Flow Induced Unsteady Loads and the Impact on Military Applications: Budapest, RTO/ AVT-123, April 25-29, 2005. 被引量:1
  • 4JONES T W, LUNSFORD C B, GRAVES S S. Design and development of a real-time model atti- tude measurement system for hypersonic facilities [C]. The 43 rd AIAA Aerospace Sciences Meet- ing, Reno: Nevada, AIAA-2005-1411, 10-13 Jan- uary 2005. 被引量:1
  • 5KVATERNIK R G, EURE K W, JUANG J. Ex- ploratory studies in generalized predictive control for active gust load alleviation[C]. NASA TM, 2006 : 214296. 被引量:1
  • 6BURNER A W, LIU T SH, DELOACH R. Un- certainty of videogrammetric techniques used for aerodynamic testing[C], The 22-d AIAA Aerody- namic Measurement Technology and Ground Tes- ting Conference St. Louis Missouri, AIAA-2002- 2794, 24-26 June 2002. 被引量:1
  • 7ROY J P, LIU T SH, BRITCHER C P. Extracting dynamic loads from optical deformation measure- ments[C]. The 47- AIAA/ASME/ASCE/AHS/ ASC Structures, Structural Dynamics and Materi- als Conference, Newport, Rhode Island, A1AA 2006-2187, 1-4 May 2006. 被引量:1
  • 8MCGOWAN A-MR, WASZAK M R. NASA's Morphing project research summaries in fiscal year 2002[C]. NASA TM-2005-213266L-18385, Feb- ruary 2005. 被引量:1
  • 9JOSEF B A D, DAFNIS A, BAARS A. et al: Aero-structural dynamics experiments at high reyn olds numbers[J]. Notes on Numerical Fluid Me- chanics and Multidisciplinary Design, 2010,109 389-424. 被引量:1
  • 10VEERMAN H P J, KANNEMANS H, JENTINKH W. High accuracy in-flight wing deformation measurements based on optical correlation tech- nique[C]. 18th SFTE (EC) Symposium, Manch- ing: Germany, 22-24 September 2008. 被引量:1

二级参考文献74

共引文献182

同被引文献121

引证文献13

二级引证文献92

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部