An Improved Range-Searching Initial Orbit-Determination Method and Correlation of Optical Observations for Space Debris

被引:4
作者
Lei, Xiangxu [1 ,2 ]
Xia, Shengfu [3 ]
Liu, Hongkang [3 ]
Wang, Xiaozhen [4 ]
Li, Zhenwei [5 ]
Han, Baomin [1 ]
Sang, Jizhang [3 ]
Zhao, You [2 ]
Luo, Hao [6 ]
机构
[1] Shandong Univ Technol, Sch Civil Engn & Geomat, Zibo 255000, Peoples R China
[2] Chinese Acad Sci, Natl Astron Observ, Beijing 100101, Peoples R China
[3] Wuhan Univ, Sch Geodesy & Geomat, Wuhan 430079, Peoples R China
[4] Xian Satellite Control Ctr, Xian 710043, Peoples R China
[5] Chinese Acad Sci, Natl Astron Observ, Changchun Observ, Changchun 130117, Peoples R China
[6] Chinese Acad Sci, Shanghai Astron Observ, Shanghai 200030, Peoples R China
来源
APPLIED SCIENCES-BASEL | 2023年 / 13卷 / 24期
关键词
space debris; optical telescope; initial orbit determination; track association; orbit determination; antisatellite;
D O I
10.3390/app132413224
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
The Changchun Observatory of the National Astronomical Observatories, Chinese Academy of Sciences, and the Shanghai Astronomical Observatory are used to generate very short arc (VSA) angle observations of objects in low Earth orbit (LEO) and geostationary orbit (GEO) with their ground-based electrical-optical telescope arrays (EA), the Changchun EA and SAO FocusGEO, respectively. These observations are used in this paper. The range-searching (RS) algorithm for initial orbit determination (IOD) is improved through the multiple combinations of observations and the dynamic range-searching step length. Two different computation modes (the normal mode and the refining mode) of the IOD computation process are proposed. The geometrical method for the association is used. The IOD and association methods are extended to the real optical observations for both LEO and GEO objects. The results show that the IOD success rate of arcs from the LEO objects is about 91%, the error of the semimajor axis (SMA) of the initial orbital elements is less than 50 km, and the correlation accuracy rate is about 89%. The IOD success rate of arcs from the GEO objects is higher than 88%, and the correlation accuracy rate is greater than 87%. The recent COSMOS 1408 antisatellite test (ASAT) generated a large amount of debris. The algorithm of this paper and the observations of Changchun EA are used to initially identify new debris, possibly from the ASAT through initial orbit determination and track association. Finally, 64 suspected new pieces of debris can be found. The results show the effectiveness of the IOD and the correlation algorithm, as well as the potential application of the optical-electrical array in studying space events.
引用
收藏
页数:14
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