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基于Gooding算法的天基光学目标跟踪定轨 被引量:3

Space-based Optical Target Determination Based on Gooding Algorithm
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摘要 开展了基于Gooding算法的400km天基平台光学目标监测的轨道确定研究,当测量误差为3"和6"时,分别对800,1500及36000km轨道高度目标进行初始轨道确定及轨道改进分析.仿真结果表明,利用400km轨道高度平台对800~1500km轨道高度目标进行初定轨,测量数据误差为3"~6"时,4~15min弧段的初定轨精度约在10km量级,1~2min弧段的初定轨精度约在100km量级;15min初定轨弧段轨道改进后误差在100m量级,弧段小于10min时轨道改进误差精度在km量级.利用400km轨道高度平台对36000km轨道高度目标进行初定轨,测量数据误差为3"时,15~20min弧段的初定轨精度约在数十km量级,8~10min弧段的初定轨精度在100km量级;轨道改进后误差在km量级.测量数据误差为6"时,20min弧段初定轨精度在10km量级,8~15min弧段初定轨精度在100km量级,轨道改进后误差精度在10km量级. In this paper,optical target monitoring orbit determination using the Gooding algorithm based on the 400km altitude space platform was researched.The measurement error was set to 3"and 6"respectively for 800km,1500km altitude low Earth orbits and 36000km altitude geosynchronous orbit to determine the initial orbit and precise orbit.Simulation results show that the initial orbit determination accuracy of the 4~15min arc is about 10km,and the 1~2min arc is about 100km when the measurement data error is between 3"and 6".The error of 15min initial determination arc is 100m.As the arc is less than 10min,the improved error accuracy of the orbit is in the order of km scale.As the measurement data error is 3",the initial orbit determination accuracy of the 15~20min arc is about tens of kilometers,and that of the 8~10min arc is 100km.The improved orbit has an error of km.When the measurement data error is 6",the accuracy of the initial orbit determination of the 20min arc is at the magnitude of 10km,the accuracy of the initial orbit determination of the 8~15min arc is at the magnitude of 100km,and the error accuracy of the improved orbit is at the magnitude of 10km.
作者 闫瑞东 王荣兰 龚建村 刘四清 师立勤 罗冰显 王宏 YAN Ruidong;WANG Ronglan;GONG Jiancun;LIU Siqing;SHI Liqin;LUO Bingxian;WANG Hong(National Space Science Center,Chinese Academy of Sciences,Beijing 100190;Innovation Academy for Microsatellites,Chinese Academy of Sciences,Shanghai 200050;Harbin Institute of Technology,Shenzhen 518055)
出处 《空间科学学报》 CAS CSCD 北大核心 2021年第2期329-336,共8页 Chinese Journal of Space Science
基金 深圳科技计划项目(JCYJ20160817172025986) 载人航天预研项目(030102)共同资助。
关键词 天基探测 光学测量 Gooding算法 初定轨 目标跟踪 Space-based observation Optical measurement Gooding algorithm IOD Target determination
作者简介 闫瑞东,E-mail:yanruidong@nssc.ac.cn。
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