| 注册
首页|期刊导航|航天器工程|GEO卫星弃置轨道稳定性分析及离轨策略优化

GEO卫星弃置轨道稳定性分析及离轨策略优化

经姚翔 杨慧

航天器工程2013,Vol.22Issue(1):21-25,5.
航天器工程2013,Vol.22Issue(1):21-25,5.DOI:10.3969/j.issn.1673-8748.2013.01.005

GEO卫星弃置轨道稳定性分析及离轨策略优化

Analysis on Stability of GEO Satellite Disposal Orbit and De-orbiting Strategy

经姚翔 1杨慧1

作者信息

  • 1. 中国空间技术研究院,北京 100094
  • 折叠

摘要

Abstract

All perturbations to GEO satellite disposal orbit are analyzed by using both analytical and numerical methods and the result of variation in perigee height of GEO satellite disposal orbit is given. With the character of 2nd order lunisolar perturbation,a new de-orbiting strategy is provided, which can ensure that the GEO satellite protected region will not be penetrated. Especially the de-orbiting strategy is applicable to the case that the disposal orbit eccentricity does not meet the requirement of GEO satellite disposal orbit as specified in IADC guideline.

关键词

GEO卫星弃置轨道/空间碎片/稳定性/偏心率

Key words

GEO satellite disposal orbit/ space debris/ stability/ eccentricity

分类

航空航天

引用本文复制引用

经姚翔,杨慧..GEO卫星弃置轨道稳定性分析及离轨策略优化[J].航天器工程,2013,22(1):21-25,5.

航天器工程

OACSTPCD

1673-8748

访问量0
|
下载量0
段落导航相关论文