首页 | 本学科首页   官方微博 | 高级检索  
     检索      

星载立体测绘相机立方镜间姿态标定
引用本文:黄桂平,钦桂勤,马开锋.星载立体测绘相机立方镜间姿态标定[J].宇航计测技术,2013,33(4):17.
作者姓名:黄桂平  钦桂勤  马开锋
作者单位:1、华北水利水电大学,郑州 450001;; 2、信息工程大学,郑州 450052
基金项目:国家863计划(2008AA042410),国家科技重大专项(2009ZX04014-093)
摘    要:介绍了测绘相机立方镜与星敏感器立方镜间坐标系转换关系的标定方法。采用4台自准直经纬仪分别对两个立方镜进行准直测量,建立立方镜坐标系,并推导了基于准直测量角度的立方镜坐标系的旋转矩阵公式;利用经纬仪间短边互瞄方法实现两个立方镜间姿态的传递。标定试验表明,该方法可以标定出两立方镜坐标轴间夹角以及测绘相机间的姿态关系,满足了相机研制要求。

关 键 词:三线阵CCD相机    立体测绘    姿态标定    立方镜    准直测量

Attitude Calibration on Three-line Array CCD Camera of Space Stereo Mapping
HUANG Gui-ping,Qin Gui-qin,MA Kai-feng.Attitude Calibration on Three-line Array CCD Camera of Space Stereo Mapping[J].Journal of Astronautic Metrology and Measurement,2013,33(4):17.
Authors:HUANG Gui-ping  Qin Gui-qin  MA Kai-feng
Institution:1、North China University of Water Resources and Electric Power, Zhengzhou 450011; 2、Institute of Geomatics,Information Engineering University, Zhengzhou 450052
Abstract:One method for calibrating the transformation matrix of cubic prism coordinate system between stereo mapping camera and star sensor was adopted. Auto collimation on two cubic prisms was finished using 4 theodolites. After that, the cubic prism coordinate system was set up. And the detailed equations of rotation matrix were deduced too. The attitude between two cubic prisms was calibrated by azimuth transmission. Tests indicate that the calibration error of angle between two cubic prism coordinate system axes is less than 1.5″(1δ). The error of final attitude calibration of the stereo mapping camera is less than 5″(1δ).
Keywords:Three-line array CCD camera                                                                                                                        Stereo mapping                                                                                                                        Attitude calibration                                                                                                                        Cubic prism                                                                                                                        Collimation measurement
点击此处可从《宇航计测技术》浏览原始摘要信息
点击此处可从《宇航计测技术》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号