首页 | 本学科首页   官方微博 | 高级检索  
     

空间跟踪技术的发展对月球重力场模型的改进
引用本文:李斐, 郝卫峰, 鄢建国, 邵先远, 叶茂, 肖驰. 空间跟踪技术的发展对月球重力场模型的改进[J]. 地球物理学报, 2016, 59(4): 1249-1259, doi: 10.6038/cjg20160407
作者姓名:李斐  郝卫峰  鄢建国  邵先远  叶茂  肖驰
作者单位:1. 武汉大学中国南极测绘研究中心, 武汉 430079; 2. 武汉大学测绘遥感信息工程国家重点实验室, 武汉 430079
基金项目:国家自然科学基金(41174019,41374024),湖北省自然科学基金重点项目创新群体类(2015CFA011),武汉大学中央高校基本科研业务费专项资金(2042014kf0051)资助.
摘    要:本文基于绕月卫星跟踪技术的三种模式,即地面跟踪模式、高低跟踪模式和低低跟踪模式,将月球重力场的发展历程分为四个阶段.分别介绍了各阶段跟踪模式的主要原理、技术特点以及所获取的具有代表性的重力场模型,并对这些模型的精度特征进行了评述.进而,通过分析不同阶段重力场模型所获取的月球重力异常特征和精度、不同阶段重力场模型的定轨精度,阐明了:空间跟踪技术的进步,极大地提高了月球重力场模型的精度,并且,有效地促进了对月球物质结构特征的认识和绕月卫星定轨的可靠性.最后对月球重力场模型中尚存在的问题以及探测技术的发展前景进行了分析和展望.

关 键 词:月球重力场   跟踪模式   内部结构   精密定轨
收稿时间:2015-10-11
修稿时间:2015-12-29

Advancement of lunar gravity model due to the development of space tracking techniques
LI Fei, HAO Wei-Feng, YAN Jian-Guo, SHAO Xian-Yuan, YE Mao, XIAO Chi. Advancement of lunar gravity model due to the development of space tracking techniques[J]. Chinese Journal of Geophysics (in Chinese), 2016, 59(4): 1249-1259, doi: 10.6038/cjg20160407
Authors:LI Fei  HAO Wei-Feng  YAN Jian-Guo  SHAO Xian-Yuan  YE Mao  XIAO Chi
Affiliation:1. Chinese Antarctic Center of Surveying and Mapping, Wuhan University, Wuhan 430079, China; 2. State Key Laboratory of Information Engineering in Surveying, Mapping and Remote Sensing, Wuhan University, Wuhan 430079, China
Abstract:Based on the three modes of lunar spacecraft tracking techniques: Earth-based tracking mode, high-low satellite-to-satellite tracking mode and low-low satellite-to-satellite tracking mode, the development of lunar gravity models could be divided into 4 stages. First, we introduce the principle, technical characteristics of the different tracking modes, and the representative gravity models, and then make comments to these models' precision. Further, through comparison of gravity anomaly precision, characteristics and orbit determination precision from different stages' lunar gravity field models, we conclude that: the advancement of space tracking techniques has significantly improved the precision of lunar gravity model and effectively promote the understanding of lunar interior structure and there liability of lunar satellite orbit determination. Finally, we analyze the deficiency of current lunar gravity models and give a perspective of future space tracking techniques.
Keywords:Lunar gravity model  Tracking mode  Lunar interior structure  Precise orbit determination
本文献已被 CNKI 等数据库收录!
点击此处可从《地球物理学报》浏览原始摘要信息
点击此处可从《地球物理学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号