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航天器相对位姿参数光学测量解析算法
引用本文:张世杰,曹喜滨,陈雪芹.航天器相对位姿参数光学测量解析算法[J].航空学报,2005,26(2):214-218.
作者姓名:张世杰  曹喜滨  陈雪芹
作者单位:哈尔滨工业大学 卫星技术研究所, 黑龙江, 哈尔滨 150001
基金项目:国家安全重大基础研究(5131201 4)资助项目
摘    要:研究了利用4个非共面特征光标和单光学测量敏感器的测量方法。基于比例正交投影近似假设,简化了光学成像数学模型,以解析的形式给出了航天器间相对位姿参数(相对位置和姿态),并对解析解进行修正。最后,对该算法进行数学仿真,仿真结果表明该算法简单可靠,能够满足航天器相对位姿确定精度和实时计算要求。

关 键 词:航天器  交会对接  光学测量  四元素  位姿确定  
文章编号:1000-6893(2005)02-0214-05
收稿时间:2004-03-16
修稿时间:2004年3月16日

Closed-Form Method for Relative Pose Parameters of Spacecraft Based on Optical Measurement
ZHANG Shi-jie,CAO Xi-bin,CHEN Xue-qin.Closed-Form Method for Relative Pose Parameters of Spacecraft Based on Optical Measurement[J].Acta Aeronautica et Astronautica Sinica,2005,26(2):214-218.
Authors:ZHANG Shi-jie  CAO Xi-bin  CHEN Xue-qin
Institution:Research Institute of Satellite Technology, Harbin Institute of Technology, Harbin 150001, China
Abstract:By using four non-coplanar reference points and an optical image sensor, this paper investigates the optical measurement method. Based on the assumption of scaled orthographic projection, the mathematical model of optical imaging is simplified by representing the relative attitude using quaternion. Then a closed-form solution is derived, and correct terms are added to obtain more accurate estimates for the pose parameters. In the last, the solution has been validated by using mathematical simulation, and simulation results show that this solution is simple and effective and the proposed solution is more suitable in on-board real-time computation.
Keywords:spacecraft  rendezvous and docking  optical measurement  quaternion  pose determination
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