期刊文献+

基于频率优化组合的KBR系统时标误差校正

A novel time-tag error correction method for KBR system based on combination of optimal frequencies
在线阅读 下载PDF
导出
摘要 时标误差是K波段精密测距仪(KBR)的一个重要测距误差源,现有的时标误差校正方法依赖于对星间时标偏差的精确测量。针对目前我国星间时标偏差测量精度不能满足校正需求的问题,提出了基于双频优化组合的时标误差校正方法,推导了优化频率之间应该满足的定量关系。研究了双频优化组合的实现,指出原有的KBR系统无法实现频率优化,在此基础上设计实现了一种改进频率流程的KBR系统,并对新的时标误差校正方法进行了实验验证。实验结果表明,基于双频优化组合的时标误差校正方法和改进的KBR系统有效降低了对星间时标偏差测量精度的要求。 Time-tag error is an important error source of K-band ranging (KBR) system, and the present methods for time-tag error correction are dependent upon accurate measurement of inter-satellite time-tag offset. Aiming at the problem that currently the national measurement accuracy of inter-satellite time-tag offset cannot satisfy the demand for time-tag error correction, a novel correction method based on the combination of two optimal frequencies is proposed, and the quantity relation of the optimal frequencies is deduced. Research on the realization for combination of two optimal frequencies, which shows that it is unrealizable utilizing the existing KBR system, was performed. Consequently, a new KBR system adopting an advanced frequency flow was designed and realized. The experimental results demonstrate that the proposed method and the advanced KBR system effectively reduce the requirement for measurement accuracy of inter-satellite time-tag offset.
出处 《国防科技大学学报》 EI CAS CSCD 北大核心 2013年第2期159-163,共5页 Journal of National University of Defense Technology
基金 国家部委资助项目
关键词 K波段精密测距仪 时标误差 频率优化组合 频率流程改进 K-band ranging system time-tag error combination of optimal frequencies advanced frequency flow
  • 相关文献

参考文献11

  • 1王正涛,姜卫平,晁定波.卫星跟踪卫星测量确定地球重力场的理论与方法[M].武汉:武汉大学出版社,2011:5.13.
  • 2Dunn C, Bertiger W, Franklin G, et al. The instrument on NASA' s GRACE mission: augmentation of GPS to achieve unprecedented gravity field measurements [ C ]//Proceeding of the 15th International Technical Meeting of the Satellite Division of the Institute of Navigation ( ION GPS 2002), Portland, OR, 2002.
  • 3Kim J, Lee S W. Flight performance analysis of GRACE K- band ranging instrument [ J ]. Acta Astronantica, 2009, 65 : 1571 - 1581.
  • 4Kim J, Lee Y J. Measurement interpolation methods for dual one-way ranging systems [ J ]. Journal of Spacecraft and Rockets, 2009, 3 : 707 - 712.
  • 5Ko U D, Tapley B D. Computing the USO frequency instability of GRACE satellites [ C ]//Proceedings of Aerospace Conference, 2010 IEEE, Big Sky, MT, 2010, 1-8.
  • 6Frommkneeht B, Sehlieht A. The GRACE gravity sensor system [ J ]. System Earth via Geodetic-Geophysical Space Techniques, Advanced Technologies in Earth Sciences, 2010, Part 2:105 -118.
  • 7佘世刚,王锴,周毅,申健,吴国富,黄欹昌.高精度星间微波测距技术[J].宇航学报,2006,27(3):402-406. 被引量:25
  • 8申健,佘世刚,王锴,何丹,黄欹昌.重力卫星星间高精度测距技术研究[J].空间科学学报,2007,27(4):342-346. 被引量:9
  • 9康开轩,李辉,邹正波,等.精密星间微波测距系统观测数据模拟与预处理技术[J].大地测量与地球动力学学报,2011,31(2):71-75.
  • 10Thomas J B. An analysis of gravity-field estimation based on inter-satellite dual-l-way biased ranging [ R ]. Jet Propulsion Lab, California Institute of Technology, JPL Publication, 1999.

二级参考文献16

  • 1Kim J,Roesset P L,Bettadpur S V,et al.Simulations of the gravity recovery and climate experiment (GRACE) mission[A].In:Proceedings of the AAS/AIAA Space Flight Mechanics Meeting[C].Breckenridge,1999,613-622
  • 2Sharma J.Precise Determination of the Geopotential with a Low-Low Satellite-to-Satellite Tracking Mission[D].Austin:The University of Texas at Austin,1995
  • 3Wolff M.Direct measurements of the earth's gravitational potential using a satellite pair[J].Journal of Geophysical Research,1969,74(22):5295-5300
  • 4Mazanek D D,Kumar R R,Seywald H,et al.GRACE mission design:impact of uncertainties in disturbance environment and satellite force models[A].In:Proceedings of the AAS/AIAA Space Flight Mechanics Meeting[C].Clearwater,2000,967-986
  • 5MacArthur J L,Posner A S.Satellite-to-satellite range-rate measurement[J].IEEE Transactions on Geosciences and Remote Sensing,1985,23(4):517-523
  • 6Thomas J B.An Analysis of Gravity-Field Estimation based on Intersatellite Dual-1-Way Biased Ranging[R].JPL Publication,California,1999
  • 7Kim J.Simulation Study of a Low-Low Satellite-to-satellite Tracking Mission[D].Austin:The University of Texas at Austin,2000
  • 8Kim J, Roesset P L, Bettadpur S Vet al. Simulations of the Gravity Recovery And Climate Experiment (GRACE) mission. In: Proceedings of the AAS/AIAA Space Flight Mechanics Meeting. Breckenridge, 1999. 613-622.
  • 9Sharma J. Precise Determination of the Geopotential With a Low-Low Satellite-to-Satellite Tracking Mission. Austin: The University of Texas at Austin, 1995.
  • 10Wolff M. Direct Measurements of the earth's gravitational potential using a satellite pair. J. Geophys. Res., 1969, 74(22):5295-5300.

共引文献30

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