摘要
提出一种基于视觉的星箭分离相对位姿测量方法。在相机内参数已知的情况下,将相机安装于运载火箭,并在卫星上固连不少于6个合作标志,利用相机对合作标志实时成像;基于单目位姿估计的基本原理,采用高效n点渗透与正交迭代结合的方式解算卫星与火箭之间的相对位姿关系。仿真实验结果、半实物仿真实验结果证明了所提测量方法的可行性和准确性。
A method of measuring the relative pose of satellite-rocket separation based on vision was presented.For the camera parameters were known,the camera was installed on the carrier rocket,and more than six cooperation signs were fixed on the satellite.The cameras can take pictures of the cooperation signs in real time.Based on the basic principle of monocular vision pose estimation,the relative pose relationship between satellite and rocket was solved by combining efficient perspective-n-point with orthogonal iteration.The simulation experiment and the semi-physical simulation experiment prove the feasibility and accuracy of the proposed method.
作者
丁少闻
陈浩
王洁
张小虎
DING Shaowen;CHEN Hao;WANG Jie;ZHANG Xiaohu(College of Aeronautics and Astronautics,National University of Defense Technology,Changsha 410073,China;Hunan Key Laboratory of Videometrics and Vision Navigation,National University of Defense Technology,Changsha 410073,China;Beijing Institute of Aerospace Systems Engineering,Beijing 100076,China;Beijing Institute of Space Mechanics&Electricity,Beijing 100094,China;School of Aeronautics and Astronautics,Sun Yat-Sen University,Guangzhou 510000,China)
出处
《国防科技大学学报》
EI
CAS
CSCD
北大核心
2018年第5期14-19,共6页
Journal of National University of Defense Technology
基金
国防科技大学科研计划资助项目(ZK16-03-27)
关键词
星箭分离
位姿估计
高效n点渗透
正交迭代
satellite-rocket separation
position and attitude estimation
efficient perspective-n-point
orthogonal iteration