| 基于立体视觉的飞行器运动姿态测量技术及其应用 |
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| 引用本文： | 温聚英,路鹰,梁雅军,张琦,陈世立.基于立体视觉的飞行器运动姿态测量技术及其应用[J].宇航计测技术,2013,33(2):12. |
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| 作者姓名： | 温聚英 路鹰 梁雅军 张琦 陈世立 |
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| 作者单位： | 1、中国运载火箭技术研究院研究发展中心，北京 100076；
2、北京航天计量测试技术研究所，北京 100076 |
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| 摘 要： | 针对某飞行器地面试验测量需求，介绍了基于立体视觉的飞行器运动姿态测量技术的基本原理和系统组成，并对其测量结果进行了分析。试验结果表明，该系统能高度准确地实时测量弹体姿态角和位置，考核了弹上制导和导航准确度，为试验的顺利完成提供了测量保障。
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| 关 键 词： | 飞行器视觉 姿态 测量 |
Measurement Technique of Motion Attitude to Vekicle Based on Stereovision and Its Application |
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| WEN Ju-ying,LU Ying,LIANG Ya-jun,ZHANG Qi,CHEN Shi-li.Measurement Technique of Motion Attitude to Vekicle Based on Stereovision and Its Application[J].Journal of Astronautic Metrology and Measurement,2013,33(2):12. |
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| Authors: | WEN Ju-ying LU Ying LIANG Ya-jun ZHANG Qi CHEN Shi-li |
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| Institution: | 1、China Academy of Launch Vehicle Technology Research and Develop Center, Beijing 100076；;
2、Beijing Aerospace Institute for Metrology and Measurement Technology, Beijing 100076 |
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| Abstract: | Aiming at the demand of spacecraft ground test, the basic principle of measurement technique based on stereovision is put forward and its system is built. The experiment results is presented that the proposed method had high accurately, and position and posture of the aerocraft are acquired. Accuracy of the navigation and control system was assessed, which ensure the accomplishment of experiment. |
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| Keywords: | Vehicle stereovision Attitude Measurement |
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