引用本文: | 李沛,罗武胜,李冠章.一种基于双目视觉原理的飞机尾旋运动姿态测量方法[J].国防科技大学学报,2008,30(2):107-111.[点击复制] |
LI Pei,LUO Wusheng,LI Guanzhang.Spin Attitude Measure Based on Stereo Vision[J].Journal of National University of Defense Technology,2008,30(2):107-111[点击复制] |
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一种基于双目视觉原理的飞机尾旋运动姿态测量方法 |
李沛, 罗武胜, 李冠章 |
(国防科技大学 机电工程与自动化学院,湖南 长沙 410073)
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摘要: |
针对飞机尾旋运动研究中的姿态测量问题,提出一种基于双目立体视差原理的测量方法。通过两部相机拍摄图像的视差,恢复模型表面特征空间三维信息,由表面特征计算模型运动姿态。设计了一组有特定形状和严格尺寸的人工特征,具有识别正确率高、定位精确等特点。提供人工特征的设计方法。最后,分别给出旋转天平实验和风洞实验的实测数据,实测结果表明该方法测量准确,鲁棒性好,在立式风洞飞机模型尾旋运动测量的应用中十分有效。 |
关键词: 飞机模型 尾旋 立体视觉 人工特征 |
DOI: |
投稿日期:2007-09-05 |
基金项目:国家部委资助项目 |
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Spin Attitude Measure Based on Stereo Vision |
LI Pei, LUO Wusheng, LI Guanzhang |
(College of Mechatronics Engineering and Automation, National Univ. of Defense Technology, Changsha 410073, China)
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Abstract: |
To measure the aircraft model attitude in the spin time, a method based on stereo vision is presented. We get the attitudes from a set of man-made signs on the surface of the model. From a pair of figures of the signs, their disparities are computed out. The design of the signs and the computation of the attitudes are presented in this paper. The man-made signs have good identifiability and the anchor points are accurate. Finally, the data of experiments to determine the aircraft model attitude are provided. Through the experiments, it can be concluded that the process of the computing is satisfactory, achieving high robustness. The measurement shows that the method discussed is useful for the experiments in the vertical wind tunnel. |
Keywords: aircraft model spin stereo vision manmade signs |
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