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基于升轨方式的低轨卫星主动离轨处置策略

张国云 樊恒海 蔡立锋 张国龙 王大鹏 祝俊淞

航天器工程2018,Vol.27Issue(2):19-25,7.
航天器工程2018,Vol.27Issue(2):19-25,7.DOI:10.3969/j.issn.1673-8748.2018.02.004

基于升轨方式的低轨卫星主动离轨处置策略

Active Deorbit Disposal Strategy for LEO Satellite Based on Orbit Elevation

张国云 1樊恒海 1蔡立锋 1张国龙 1王大鹏 1祝俊淞1

作者信息

  • 1. 西安卫星测控中心,西安 710043
  • 折叠

摘要

Abstract

In light of the problems of too long orbit decay time and collision risk in LEO (low earth orbit)satellite deorbit,an active deorbit disposal strategy based on orbit elevation is pro-posed.In this strategy,the satellite orbit is elevated to safe orbit by several Homan orbital trans-fer.The proposed coordination strategy of"energy maintenance,propellant maintenance,mea-surement and control maintenance"meets the needs of safe operation,emergency treatment and scientific test through the adj ustment of satellite attitude and the angular velocity after deorbit. The test results of a retired LEO satellite show that the active deorbit disposal strategy is reason-able and effective,and satellite data on orbit show that the satellite spins steadily around the main axis of inertia with adequate energy and stable tracking control.The active deorbit disposal strategy proposed in the paper provides useful references for deorbit disposal of LEO satellites in higher orbit.

关键词

低轨卫星/主动离轨/升轨方式/自旋稳定

Key words

LEO satellite/active deorbit/orbit elevation/spin-stabilization

分类

航空航天

引用本文复制引用

张国云,樊恒海,蔡立锋,张国龙,王大鹏,祝俊淞..基于升轨方式的低轨卫星主动离轨处置策略[J].航天器工程,2018,27(2):19-25,7.

航天器工程

OA北大核心CSCDCSTPCD

1673-8748

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