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


Space Event and Outlier Detection Based on Expectation Maximization Algorithm
Institution:1. Smart City Institute, Chongqing Jiaotong University, Chongqing 400074, China;2. Purple Mountain Observatory, Chinese Academy of Sciences, Nanjing 210023, China;3. School of Civil and Architectural Engineering, Shandong University of Technology, Zibo 255000, China;1. School of Computer Science and Technology, Xi’an University of Posts and Telecommunications, Xi’an 710121, China;2. School of Electrical and Electronic Engineering, Baoji University of Arts and Sciences, Baoji 721016, China;3. National Time Service Center, Chinese Academy of Sciences, Xi’an 710600, China;4. SPBPU Institute of Engineering, Jiangsu Normal University, Xuzhou 221116, China;1. National Astronomical Observatories, Chinese Academy of Sciences, Beijing 100101, China;2. University of Chinese Academy of Sciences, Beijing 100049, China;3. Lunar Exploration and Space Engineering Center, Beijing 100190, China
Abstract:The United States provide Element Sets (ELSET) database in Two-Line Element (TLE) format for public use, which plays an important role in the inversion of atmospheric density in the thermosphere, ballistic coefficient estimation, early-warning and so on. Due to large uncertainties existing in the TLE generation process, space environment changes, and space events, ELSET database contains a large number of abnormal TLE data to be filtered, such as corrected TLE, orbital element outlier, and Bstar outlier. The existing methods to filter out the outliers lack general applicability and are very complicated, which are only applicable to a few space targets in certain orbit regions. To overcome the shortcomings of the existing methods, a filtering method is proposed based on Expectation Maximization (EM) algorithm employing a sliding window and polynomial fitting method, which can detect outliers for different orbital elements and space events. The research shows that the algorithm can effectively single out the outliers in TLE sequences and is suitable for all orbital debris.
Keywords:
本文献已被 ScienceDirect 等数据库收录!
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