基于立体视觉的飞行器运动姿态测量技术及其应用  

Measurement Technique of Motion Attitude to Vekicle Based on Stereovision and Its Application

作　　者：温聚英[1] 路鹰[1] 梁雅军[2] 张琦[1] 陈世立[1] 

机构地区：[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

出　　处：《宇航计测技术》2013年第2期12-15,21,共5页Journal of Astronautic Metrology and Measurement

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。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 experi- ment.

关 键 词：飞行器视觉 姿态 测量 

分 类 号：V416[航空宇航科学与技术—航空宇航推进理论与工程]