Orbit determination and thrust force modeling for a maneuvered GEO satellite using two-way adaptive Kalman filtering

Author:

Xu TianHe,He KaiFei,Xu GuoChang

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy

Reference17 articles.

1. Carolipio E, Pandya N. GEO orbit determination via covariance analysis with a known clock error. ION GPS 2001, Salt Lake City, UT, 2001. 2360–2365

2. Grewal M. Comparison of GEO and GPS orbit determination. ION GPS 2002, Portland, OR, 2002. 790–799

3. Guo R, Hu X G, Tang B, et al. Precise orbit determination for geostationary satellites with multiple tracking techniques. Chin Sci Bull, 2010, 55(8): 687–692

4. He K F, Xu T H. Kinematic orbit determination of GEO satellite based on Kalman filtering. J Geod Geodyn, 2009, 29(6): 109–114

5. Huang Y, Hu X G, Huang C, et al. Precise orbit determination of a maneuvered GEO satellite using CAPS ranging data. Sci China Ser G-Phys Mech Astron, 2009, 52(6): 346–352

Cited by 13 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3