检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:鲁荣荣 孙海波 付双飞[1,2,4] 朱枫[1,2,4] 郝颖明[1,2,4] LuRongrong;Sun Haibo;FuShuangfei;Zhu Feng;HaoYingming(Shenyang Institute of Automation ,Chinese Academy of Sciences,Shenyang, Liaoning 110016,China;Institutes for Robotics and Intelligent Manufacturing,Chiyiese Academy of Sciences,Shenyang,Liaoning W0016,China;University of Chinese Academy of Sciences,Beijing 100049,China;Key Laboratory of Opto-Electrcmic Inform ation Process, Chinese Academy of Sciences,Shenyang,Liaoning 110016,China;Faculty of Robot Science and Engineering,Northeastern University,Shenyaiig,Liaoning 110819,China)
机构地区:[1]中国科学院沈阳自动化研究所,辽宁沈阳110016 [2]中国科学院机器人与智能制造创新研究院,辽宁沈阳110016 [3]中国科学院大学,北京100049 [4]中国科学院光电信息处理重点实验室,辽宁沈阳110016 [5]东北大学机器人科学与工程学院,辽宁沈阳110819
出 处:《激光与光电子学进展》2019年第14期203-212,共10页Laser & Optoelectronics Progress
基 金:创新基金(CXJJ-17S032)
摘 要:为了实现空间翻滚卫星(同时作自旋和进动的卫星)的消旋,提出了一种非接触式的卫星运动参数辨识方法。算法主要包含3个步骤:通过点云配准技术,获取相邻两幅点云之间的位姿变换关系,从而可以依据这些位姿变换得到卫星点云中每个点的运动轨迹;基于自旋轴上的点只绕进动轴旋转的特点,借助主成分分析与圆拟合的方式,搜索自旋轴上的点并确定进动轴的方向和位置;根据整体位姿变换与两种运动间的关系,建立非线性方程组求解出翻滚卫星的运动参数。仿真实验结果表明,在一定的噪声程度下,所提方法可以准确地辨识出空间翻滚卫星的运动参数。A non-contact satellite motion param eter identification method is proposed for the derotation of satellites that roll in space while simultaneously spinning and precessing. The algorithm involves three main steps. First, the point-cloud registration is used to obtain the pose transform ation between two adjacent point clouds, from which the trajectories of the points in the satellite's point cloud are obtained. Second, because the points on the spin axis only rotate around the moving axis, the principal component analysis and circle-fitting method are used to find a point on the spin axis and thereby determine the direction and position of the precession axis. Finally, the rolling satellite's param eters are found by solving a set of nonlinear equations, established based on the relationships between the overall pose transform ation and the two motions. The simulation results show that the proposed method can accurately identify the motion param eters of a rolling satellite for certain noise levels.
关 键 词:机器视觉 点云配准 卫星消旋 参数辨识 运动估计
分 类 号:TP391[自动化与计算机技术—计算机应用技术]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:216.73.216.222