Optics and Precision Engineering, Volume. 30, Issue 4, 455(2022)
Research on attitude measurement technology of free flying model under window distortion correction
[1] [1] 1孙海生, 岑飞, 聂博文, 等. 水平风洞模型自由飞试验技术研究现状及展望[J]. 实验流体力学, 2011, 25(4): 103-108. doi: 10.3969/j.issn.1672-9897.2011.04.020SUNH S, CENF, NIEB W, et al. Present research status and prospective application of wind-tunnel free-flight test technique[J]. Journal of Experiments in Fluid Mechanics, 2011, 25(4): 103-108.(in Chinese). doi: 10.3969/j.issn.1672-9897.2011.04.020
[2] [2] 2范洁川. 风洞试验手册[M]. 北京: 航空工业出版社, 2002.FANJ C. Handbook of Wind Tunnel Test[M]. Beijing: Aviation Industry Press, 2002.(in Chinese)
[3] [3] 3蒋增辉, 宋威, 鲁伟. 高速风洞模型自由飞试验技术[J]. 空气动力学学报, 2017, 35(5): 680-686, 692. doi: 10.7638/kqdlxxb-2016.0101JIANGZ H, SONGW, LUW. High-speed wind tunnel free-flight test technique[J]. Acta Aerodynamica Sinica, 2017, 35(5): 680-686, 692.(in Chinese). doi: 10.7638/kqdlxxb-2016.0101
[4] [4] 4李周复. 风洞特种试验技术[M].北京:航空工业出版社, 2010: 328-353.LIZ F. Special Test Technology in Wind Tunnel[M]. Beijing: Aviation Industry Press, 2010: 328-353. (in Chinese)
[5] M HOLDEN, G SMOLINSKI, E MUNDY et al. Experimental studies for hypersonic vehicle design and code validation of unsteady flow characteristics associated with “free flight” shroud and stage seperation, and mode switching, 642(07).
[6] [6] 6贾区耀, 杨益农, 蒋增辉. 风洞自由飞实验结果的精度、准度[J]. 宇航学报, 2009, 30(6): 2082-2085. doi: 10.3873/j.issn.1000-1328.2009.06.005JIAQ Y, YANGY N, JIANGZ H. The precision and accuracy of wind tunnel free-flight experiment result[J]. Journal of Astronautics, 2009, 30(6): 2082-2085.(in Chinese). doi: 10.3873/j.issn.1000-1328.2009.06.005
[7] [7] 7李桂春. 风洞试验光学测量方法[M]. 北京: 国防工业出版社, 2008.LIG C. Optical Instrumentation for Wind Tunnel Testing[M]. Beijing: National Defense Industry Press, 2008.(in Chinese)
[8] [8] 8张天姣, 汪清, 何开锋, 等. 风洞自由飞试验中气动参数辨识准度评价方法研究[J]. 实验流体力学, 2017, 31(1): 39-46. doi: 10.11729/syltlx20160148ZHANGT J, WANGQ, HEK F, et al. Research on accuracy assessment method of aerodynamic parameters identified from wind tunnel free-flight test data[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(1): 39-46.(in Chinese). doi: 10.11729/syltlx20160148
[9] [9] 9张施豪, 吴文启, 何晓峰, 等. 基于MEMS陀螺的风洞模型水平姿态动态测量与精度评估[J]. 导航与控制, 2018, 17(6): 86-93. doi: 10.3969/j.issn.1674-5558.2018.06.014ZHANGS H, WUW Q, HEX F, et al. Wind tunnel model horizontal attitude dynamic measurement and precision evaluation based on MEMS gyros[J]. Navigation and Control, 2018, 17(6): 86-93.(in Chinese). doi: 10.3969/j.issn.1674-5558.2018.06.014
[10] J WEISS. Model vibrations and inertial bias measurement in a transonic wind tunnel test(2008).
[11] [11] 11宋晋, 蒋敏, 李睿, 等. 基于MEMS传感器的风洞尾旋姿态测量研究[J]. 计算机测量与控制, 2016, 24(12): 1-2, 13. doi: 10.1109/icfst.2017.8210485SONGJ, JIANGM, LIR, et al. Attitude measurement of spin in wind tunnel based on MEMS sensor[J]. Computer Measurement & Control, 2016, 24(12): 1-2, 13.(in Chinese). doi: 10.1109/icfst.2017.8210485
[12] [12] 12周凡桂, 王晓光, 高忠信, 等. 双目视觉绳系支撑飞行器模型位姿动态测量[J]. 航空学报, 2019, 40(12): 123059.ZHOUF G, WANGX G, GAOZ X, et al. Binocular vision-based measurement of dynamic motion for aircraft model suspended by wire system[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(12): 123059.(in Chinese)
[13] [13] 13骆敬. 基于双目视觉的靶场飞行目标位姿测量方法研究[D]. 长沙: 国防科技大学, 2017.LUOJ. Research on Position and Pose Estimation of Flight Target in Range Based on Binocular Vision[D]. Changsha: National University of Defense Technology, 2017. (in Chinese)
[14] [14] 14谢明伟, 盖文, 褚卫华, 等. 基于双目立体视觉的风洞模型姿态测量研究[J]. 测控技术, 2016, 35(12): 34-37. doi: 10.3969/j.issn.1000-8829.2016.12.008XIEM W, GAIW, CHUW H, et al. Binocular stereopsis system for model attitude measurement in wind tunnels[J]. Measurement & Control Technology, 2016, 35(12): 34-37.(in Chinese). doi: 10.3969/j.issn.1000-8829.2016.12.008
[15] [15] 15张建德, 陆金桂. 双目视觉三维数字化测量技术研究[J]. 组合机床与自动化加工技术, 2011(2): 1-4, 9. doi: 10.3969/j.issn.1001-2265.2011.02.001ZHANGJ D, LUJ G. Summary of research on binocular stereo vision 3D measurement technique[J]. Modular Machine Tool & Automatic Manufacturing Technique, 2011(2): 1-4, 9.(in Chinese). doi: 10.3969/j.issn.1001-2265.2011.02.001
[16] [16] 16李桂春. 气动光学[M]. 北京: 国防工业出版社, 2006.LIG C. Aero-optics[M]. Beijing: National Defense Industry Press, 2006.(in Chinese)
[17] [17] 17张广军. 机器视觉[M]. 北京: 科学出版社, 2005.ZHANGG J. Machine Vision[M]. Beijing: Science Press, 2005.(in Chinese)
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Lei CHEN, Yang XU, Xiaobin XU, Tao ZHU, Xiaoyu MA, Fei XIE, Chao HE. Research on attitude measurement technology of free flying model under window distortion correction[J]. Optics and Precision Engineering, 2022, 30(4): 455
Category: Information Sciences
Received: Jun. 2, 2021
Accepted: --
Published Online: Mar. 4, 2022
The Author Email: XU Yang (mingze0108@126.com)