期刊文献+

“嫦娥二号”卫星拓展试验轨道计算中心天体的选取 被引量:2

Selection of Integration Center for Chang′e-2 Satellite Extended Mission
下载PDF
导出
摘要 飞行器的星历积分不可避免涉及中心天体的选取问题。"嫦娥二号"卫星在拓展试验期间处于弱引力区,文章针对拓展试验期间的轨道状态,从受摄运动二体问题角度分析得出适宜选取太阳作为中心天体。进而结合真实力模型情况,使用行星星历表计算行星产生的摄动力,从理论上推导得出在忽略小天体摄动的前提下,由于摄动天体同时对中心天体和飞行器产生摄动作用,以地球为中心天体产生的摄动力类似于潮汐力,而以太阳为中心天体则不然,因而更适宜选取地球作为中心天体计算轨道运动问题。 The selection of integration center is inevitably involved in the orbital spacecraft calculation, so it is for Changle-2 (CE-2) mission. During its extended mission, CE-2 satellite was placed in the Sun-Earth L2 libration orbit near the weak gravitational area. The selection of the integration center was discussed with theoretical analysis. According to the perturbed two-body problem, it is appropriate to choose the Sun as the integration center. While the force model was calculated by using the JPL DE ephemeris without considering the perturbation of small planets, the Earth would appear to be a better choice.
出处 《中国空间科学技术》 EI CSCD 北大核心 2013年第2期13-18,共6页 Chinese Space Science and Technology
基金 国家自然科学基金(11173005 11073047 11203003)资助项目
关键词 星历积分 中心天体 摄动二体问题 拓展试验 “嫦娥二号”卫星 Orbit integration Central body Perturbed two-body problem Extended mission Chang'e-2 satellite
  • 相关文献

参考文献9

  • 1刘林著..航天器轨道理论[M].北京:国防工业出版社,2000:621.
  • 2TAPLEY B D, SCHUTZ B E, GEORGE H B. Statistical orbit determination [M]. California: Elsevier Academic Press, 2004.. 44-87. 被引量:1
  • 3LUTHCKE S B, ZELENSKY N P, ROWLANDS D D, et al. The 1-Centimeter orbit: Jason-1 precision orbit determination using GPS, SLR, DORIS, and altimeter data [J]. Marine Geodesy, 2003, 26(3): 399-421. 被引量:1
  • 4陈明,张宇,曹建峰,李勰,唐歌实,王健,段建锋,谢剑锋,童斌.嫦娥二号卫星轨道确定与测轨技术[J].科学通报,2012,57(9):689-696. 被引量:38
  • 5WU WeiRen,LIU Yong,LIU Lei,ZHOU JianLiang,TANG GeShi,CHEN YongZhi.Pre-LOI trajectory maneuvers of the CHANG'E-2 libration point mission[J].Science China(Information Sciences),2012,55(6):1249-1258. 被引量:13
  • 6BECKMAN M. Orbit determination issues for libration point orbits [C]//Libration Point Orbits And Applications Proceeding, Spain, Singapore: World Scientific Publishing, 2003: 1-18. 被引量:1
  • 7GODARD B, CROON M, BUDNIK F, et al. Orbit determination of the planck satellite [C]. 21^st International Symposium on Space Flight Dynamics, Toulouse, 2009; 1-15. 被引量:1
  • 8STANDISH E M. JPL planetary ephemeris DE414, IOM 343R-06 002 [R]. California: Jet Propulsion Laboratory, 2006: 1-8. 被引量:1
  • 9FOLKNER W M, WILLIAMS J G, BOGGS D H. The planetary and lunar ephemeris DE421, IOM 343R-08-003 [R]. California: Jet Propulsion Laboratory, 2008: 1-31. 被引量:1

二级参考文献9

共引文献47

同被引文献25

引证文献2

二级引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部