中国科学院紫金山天文台机构知识库
Advanced  
PMO OpenIR  > 空间目标与碎片观测研究基地  > 期刊论文
题名: Analysis on the long-term dynamical evolution of the inclined geosynchronous orbits in the Chinese BeiDou navigation system
作者: Zhao, Chang-Yin1, 2; Zhang, Ming-Jiang1, 2, 3; Wang, Hong-Bo1, 2; Xiong, Jian-Ning1, 2; Zhu, Ting-Lei1, 2, 3; Zhang, Wei1, 2
刊名: ADVANCES IN SPACE RESEARCH
出版日期: 2015-08-01
卷号: 56, 期号:3, 页码:377-387
关键词: Long-term dynamical evolution ; Inclined geosynchronous orbit ; Chinese BeiDou navigation system ; Mitigation strategy
学科分类: 天文和天体物理
DOI: 10.1016/j.asr.2015.01.007
文章类型: Article
英文摘要: Five inclined geosynchronous orbit (IGSO) satellites with the inclination of about 55 degrees in the Chinese BeiDou navigation system have been put in orbit until now. The Inter-Agency Space Debris Coordination Committee (IADC) has defined a geosynchronous orbit (GEO) protected region and recommended that the GEO satellite should be maneuvered to a disposal orbit high enough at end-of-mission to remain above the GEO protected region. The recommended disposal altitude is at least 235 km + (1000. C-R . A/M) higher than the perigee altitude of the GEO satellite, where C-R and A/M are radiation pressure coefficient and area-to-mass ratio respectively. Whether this recommendation is also adequate for the disposal of these IGSO satellites in the Chinese BeiDou navigation system at end-of-mission? And if not, is there any other possible strategy to do? In view of these considerations, the long-term dynamical evolution of these IGSO satellites is investigated by both theoretical analysis and numerical computation methods in this paper. Some qualitative orbital evolution characteristics and quantitative result of variation ranges of the semi-major axis a, the inclination i and the eccentricity e are presented respectively. Based on these results, a possible mitigation strategy to reduce the orbital lifetime of the IGSO satellites after end-of-mission is proposed. (C) 2015 COSPAR. Published by Elsevier Ltd. All rights reserved.
WOS标题词: Science & Technology ; Physical Sciences
类目[WOS]: Astronomy & Astrophysics ; Geosciences, Multidisciplinary ; Meteorology & Atmospheric Sciences
研究领域[WOS]: Astronomy & Astrophysics ; Geology ; Meteorology & Atmospheric Sciences
关键词[WOS]: RESONANT LUNISOLAR PERTURBATIONS ; EARTH SATELLITE ORBITS ; CIRCULAR ORBIT ; SPACE DEBRIS ; PLANE ; INCLINATION ; MOTION
收录类别: SCI
所属项目名称: PMO_LIB-IR
语种: 英语
WOS记录号: WOS:000357905200003
Citation statistics:
内容类型: 期刊论文
URI标识: http://libir.pmo.ac.cn/handle/332002/14812
Appears in Collections:空间目标与碎片观测研究基地_期刊论文

Files in This Item:
File Name/ File Size Content Type Version Access License
2015032.pdf(1735KB)----限制开放View 联系获取全文

作者单位: 1.Chinese Acad Sci, Purple Mt Observ, Nanjing 210008, Jiangsu, Peoples R China
2.Chinese Acad Sci, Purple Mt Observ, Key Lab Space Object & Debris Observat, Nanjing 210008, Jiangsu, Peoples R China
3.Univ Chinese Acad Sci, Beijing 100049, Peoples R China
Service
Recommend this item
Sava as my favorate item
Show this item's statistics
Export Endnote File
Google Scholar
Similar articles in Google Scholar
[Zhao, Chang-Yin]'s Articles
[Zhang, Ming-Jiang]'s Articles
[Wang, Hong-Bo]'s Articles
CSDL cross search
Similar articles in CSDL Cross Search
[Zhao, Chang-Yin]‘s Articles
[Zhang, Ming-Jiang]‘s Articles
[Wang, Hong-Bo]‘s Articles
Related Copyright Policies
Null
Social Bookmarking
Add to CiteULike Add to Connotea Add to Del.icio.us Add to Digg Add to Reddit
文件名: 2015032.pdf
格式: Adobe PDF
所有评论 (0)
暂无评论
 
评注功能仅针对注册用户开放,请您登录
您对该条目有什么异议,请填写以下表单,管理员会尽快联系您。
内 容:
Email:  *
单位:
验证码:   刷新
您在IR的使用过程中有什么好的想法或者建议可以反馈给我们。
标 题:
 *
内 容:
Email:  *
验证码:   刷新

Items in IR are protected by copyright, with all rights reserved, unless otherwise indicated.

 

 

Valid XHTML 1.0!
Copyright © 2007-2018  中国科学院紫金山天文台 - Feedback
Powered by CSpace