期刊文献+

伪码辅助载波星间自主测距技术 被引量:1

A Pseudo-random Code-Aided Carrier-Based Inter-Satellite Autonomous Ranging Technique
下载PDF
导出
摘要 提出了一种存在弱相对运动的卫星之间基于载波高精度自主相对测距技术,它借助伪码测距技术所得到的粗测距离和cm级测距精度选择载波频率,消除了载波测距中存在的整周模糊度问题,避开了复杂的整周模糊度求解算法;借助伪码高精度时间差测量技术,使不同卫星上面伪码和载波相位观测时间之差的测量精度(标准偏差)优于0.1ns,并使得星间钟差可忽略不计。最终测距3σ精度有基于伪码的cm级提高到了mm级。文中不仅分析了相对静止时卫星间的距离测量精度,而且分析了存在弱相对运动(相对运动速度不大于10m/s)时卫星间距离测量精度。理论分析和工程可实现性分析都表明:该技术切实可行且易于实现。 A novel inter-satellite autonomous ranging technique based on carrier is proposed in the case of weak relative motion.With the help of the pseudo-random code,a coarse range measurement value with low accuracy but without ambiguity can be gotten.The coarse measurements with low accuracy are used to select the carrier frequencies to make the carrier-cycle integer ambiguity vanish in case the carrier-based ranging is used.in case the carrier-based ranging is used.The proposed carrier-based ranging technique is used to measure the distance again and the measurement accuracy can reach to the millimeter-level from the centimeter-level reached by the code-based method.This paper analyses the measurement accuracy in both relative stationary and motional cases,and the results show this novel ranging technique is practicable and easy to be implemented.
出处 《宇航学报》 EI CAS CSCD 北大核心 2010年第6期1618-1624,共7页 Journal of Astronautics
关键词 星间测距 载波测距 伪码测距 整周模糊度 Inter-satellite ranging Carrier-based ranging Pseudo-random code-based ranging Carrier-cycle integer ambiguity
  • 相关文献

参考文献4

  • 1Kim J,Tapley B D.Simulation of dual one-way ranging measurements[J].Journal of Spacecraft and Rockets,2003,40(3):419-425.
  • 2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
  • 3Kapalan E D,Hegarty C J,et al.Understanding GPS:printciples and applications[M].Second Edition,London:Artech House,2006.
  • 4Mistra P,Enge P,et al.Global positioning system-signals,measurements and performance[M].Second Edition,USA:Ganga-Jamuma Press,2006.

二级参考文献9

  • 1Kim 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.
  • 2Sharma J. Precise Determination of the Geopotential With a Low-Low Satellite-to-Satellite Tracking Mission. Austin: The University of Texas at Austin, 1995.
  • 3Wolff M. Direct Measurements of the earth's gravitational potential using a satellite pair. J. Geophys. Res., 1969, 74(22):5295-5300.
  • 4Watkins M M, Folkner W M, Chao B, Tapley B D. Ex-5: A laser interferometer mission follow-on to the GRACE mission. In: IAG International Symposium. Banff, 2000.
  • 5Thomas J B. An Analysis of Gravity-Field Estimation Based on Inter-satellite Dual-1-Way Biased Ranging. California: JPL Publication, 1999.
  • 6MacArthur J L, Posner A S. Satellite-to-satellite rangerate measurement. IEEE Trans. Geosci. Remote Sensing, 1985, 23(4):517-523.
  • 7Kim J. Simulation Study of a Low-Low Satellite-toSatellite Tracking Mission. Austin: The University of Texas at Austin, 2000.
  • 8Leitch J, Craig R, Bender P et al. Laboratory demonstration of low Earth orbit inter-satellite interferometric ranging. In: Conference on lasers and electro-optics, Optical Society of America, 2005. 1754-1756.
  • 9Bender P, Hall J L, Ye Jet al. Satellite-satellite laser links for future gravity missions. Space Sci. Rev., 2003, 108:377-384.

共引文献8

同被引文献12

引证文献1

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