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嫦娥一号绕月探测器轨道投入过程实时监测判定的原理与技术实现

平劲松 王明远 史弦 简念川

空间科学学报2011,Vol.31Issue(3):330-337,8.
空间科学学报2011,Vol.31Issue(3):330-337,8.

嫦娥一号绕月探测器轨道投入过程实时监测判定的原理与技术实现

Real Time Monitoring the Orbit Insertion of Chang'E-1 Lunar Mission

平劲松 1王明远 1史弦 2简念川1

作者信息

  • 1. 中国科学院上海天文台,上海200030
  • 2. 中国科学院研究生院,北京100049
  • 折叠

摘要

Abstract

China's first lunar satellite Chang'E-1 (CE-1) was launched on Oct.24, 2007.During its flight to the Moon, a series of maneuvers were performed to keep the satellite in the correct trajectory.Among these maneuvers, the one performed for Lunar Orbit Insertion (LOI) was the most important part since it directly decided whether the satellite could enter the mission orbit or not.Therefore,real time monitoring and estimation of the satellite's state during this stage became crucial.A system was develop for LOI monitoring using as few data as possible.This system included real time data transmission as well as real time data analysis which could provide the difference between the predicted and observed measurements in the first place, and then, most importantly, it also gives the ensuing orbit insertion conditions, i.e.predicts probable future orbit parameters after the maneuver.The presented method was successfully applied for the LOI process in the mission phase.

关键词

嫦娥一号/轨道机动/近月点制动/实时监测系统

Key words

Chang'E-1/Lunar Orbit Insertion (LOI)/ Monitoring/ Maneuver

分类

航空航天

引用本文复制引用

平劲松,王明远,史弦,简念川..嫦娥一号绕月探测器轨道投入过程实时监测判定的原理与技术实现[J].空间科学学报,2011,31(3):330-337,8.

基金项目

国家自然科学基金项目(10973031),中国绕月探测工程项目,国家高技术研究发展计划高新(2008AA12A210,2009AA12206)和中国科学院方向性项目(KJCX2-YW-T13-2)共同资助 (10973031)

空间科学学报

OA北大核心CSCDCSTPCD

0254-6124

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