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高精度星间测距与超稳振荡器研究 被引量:1

The Study of High Accuracy Inter-satellite Ranging Technology and Ultra Stable Oscillator
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摘要 高精度K频段微波星间测距系统(KBR)采用双路微波测距技术,测量精度可达到1μm/s,是地球重力场测量卫星的三大有效载荷之一。作为整个系统时间基准的超稳定振荡器(USO),是实现KBR微米级测量精度的关键。文章在研究KBR测距技术的基础上,对USO进行了研究和设计,研制成功的USO的短期频率稳定度达到了5×10-13/s(Allan方差),达到了指标要求。 The accuracy of high accuracy KBR system (K Band Ranging System)could reach 1 μm/s based on dual-one-way microwave-ranging technology. The KBR system is one of the three major payload of gravity field measurement satellite. As the frequency time standard of the whole system, the USO( Ultra-stable oscillators)is the key technology for the measurement accuracy. Based on study of the KBR ranging technology, the USO is researched and designed. The short-term frequency stability of the successfully developed USO, have reached 5 × 10^-13/s (Allan deviations),which can completely met the requirement of this system.
出处 《空间电子技术》 2011年第1期56-64,共9页 Space Electronic Technology
关键词 高精度星间测距系统 KBR 超稳振荡器 USO 稳定度 High accuracy inter-satellite ranging system KBR( K Band Ranging System) USO(Ultra-sta- ble oscillators) Stability
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  • 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. 被引量:1
  • 2MacArthur J L, Posner A S. Satellite-to-satellite range- rate measurement[J]. IEEE Trans. on Geosciences and Remote Sensing, 1985, 23(4) : 517 -523. 被引量:1
  • 3Mazanek D D, Kumar R R, Seywald H, et al. GRACE mission design : impact of uncertainties in disturbance en- vironment and satellite force models[ A]. In: Proceed- ings of the AAS/AIAA Space Flight Mechanics Meeting [ C ]. Clearwater, 2000, 967-986. 被引量:1
  • 4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:24
  • 5Wolff M. Direct measurements of the earth's gravitational potential using a satellite pair[J]. Journal of Geophysical Research, 1969, 74(22): 5295-5300. 被引量:1
  • 6Thomas J B. An analysis of gravity-field estimation based on inter-satellite dual-l-Way biased ranging [ R ]. JPL Publication, California, 1999. 被引量:1
  • 7Kim J. Simulation study of a low-low satellite-to-satellite tracking mission[ D]. Austin: The University of Texas at Austin, 2000. 被引量:1
  • 8余世刚.高精度K频段星间微波测距技术研究[D].兰州:兰州大学,2006. 被引量:1
  • 9臧其源,林时昌编著..振荡器的频率稳定度及其对电子系统的影响[M].北京:宇航出版社,1990:307.
  • 10Norton J R, Cloeren J M. Brief history of the develop- ment of ultra-precise osciliators for ground and space ap- plications [ C ]. 1996 IEEE International Frequency Con- trol Symposium, 1996, 47 - 57. 被引量:1

二级参考文献13

  • 1郑筱霞.SC切小型高稳定晶体振荡器的研制[J].苏州大学学报(自然科学版),1989,5(3):271-274. 被引量:1
  • 2赖寿宏.微型计算机控制技术[M].北京:机械工业出版社,1997.50-62. 被引量:8
  • 3张志涌 等.精通Matlab 6.5版[M].北京:北京航空航天出版社,2003.. 被引量:109
  • 4Kim 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 被引量:1
  • 5Sharma J.Precise Determination of the Geopotential with a Low-Low Satellite-to-Satellite Tracking Mission[D].Austin:The University of Texas at Austin,1995 被引量:1
  • 6Wolff M.Direct measurements of the earth's gravitational potential using a satellite pair[J].Journal of Geophysical Research,1969,74(22):5295-5300 被引量:1
  • 7Mazanek 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 被引量:1
  • 8MacArthur J L,Posner A S.Satellite-to-satellite range-rate measurement[J].IEEE Transactions on Geosciences and Remote Sensing,1985,23(4):517-523 被引量:1
  • 9Thomas J B.An Analysis of Gravity-Field Estimation based on Intersatellite Dual-1-Way Biased Ranging[R].JPL Publication,California,1999 被引量:1
  • 10Kim J.Simulation Study of a Low-Low Satellite-to-satellite Tracking Mission[D].Austin:The University of Texas at Austin,2000 被引量:1

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