期刊文献+

Dual transponder ranging performance in the presence of oscillator phase noise 被引量:1

Dual transponder ranging performance in the presence of oscillator phase noise
下载PDF
导出
摘要 A dual transponder carrier ranging method can be used to measure inter-satellite distance with high precision by combining the reference and the to-and-fro measurements. Based on the differential techniques, the oscillator phase noise, which is the main error source for microwave ranging systems, can be significantly attenuated. Further, since the range measurements are derived on the same satellite, the dual transponder ranging system does not need a time tagging system to synchronize the two satellites. In view of the lack of oscillator noise analysis on the dual transponder ranging model, a comprehensive analysis of oscillator noise effects on ranging accuracy is provided. First, the dual transponder ranging system is described with emphasis on the detailed analysis of oscillator noise on measurement precision. Then, a high-fidelity numerical simulation approach based on the power spectrum density of an actual ultra-stable oscillator is carried out in both frequency domain and time domain to support the presented theoretical analysis. The simulation results under different conditions are consistent with the proposed concepts, which makes the results reliable. Besides, the results demonstrate that a high level of accuracy can be achieved by using this oscillator noise cancelation-oriented ranging method. A dual transponder carrier ranging method can be used to measure inter-satellite distance with high precision by combining the reference and the to-and-fro measurements. Based on the differential techniques, the oscillator phase noise, which is the main error source for microwave ranging systems, can be significantly attenuated. Further, since the range measurements are derived on the same satellite, the dual transponder ranging system does not need a time tagging system to synchronize the two satellites. In view of the lack of oscillator noise analysis on the dual transponder ranging model, a comprehensive analysis of oscillator noise effects on ranging accuracy is provided. First, the dual transponder ranging system is described with emphasis on the detailed analysis of oscillator noise on measurement precision. Then, a high-fidelity numerical simulation approach based on the power spectrum density of an actual ultra-stable oscillator is carried out in both frequency domain and time domain to support the presented theoretical analysis. The simulation results under different conditions are consistent with the proposed concepts, which makes the results reliable. Besides, the results demonstrate that a high level of accuracy can be achieved by using this oscillator noise cancelation-oriented ranging method.
出处 《Journal of Central South University》 SCIE EI CAS CSCD 2015年第4期1350-1357,共8页 中南大学学报(英文版)
基金 Project(61106113)supported by the National Natural Science Foundation of China
关键词 inter-satellite carrier ranging oscillator phase noise power spectral density high precision 相位噪声 振荡器 转发 测距性能 数值模拟方法 距离测量 测距系统 测距方法
  • 相关文献

参考文献2

二级参考文献26

  • 1Aguirre, S., Hurd, W.J., 1984. Design and Performance of Sampled Date Loops for Subcarrier and Carrier Tracking. The Telecommunications and Data Acquisition Progress Report 42-79, Jet Propulsion Laboratory, Pasadena, Calif.
  • 2Bertiger, W., Bar-Sever, Y., Desai, S., Dunn, C., 2002. GRACE: Millimeters and Microns in Orbit. Proc. ION GPS, Institute of Navigation, p.2022-2029.
  • 3Bertiger, W., Dunn, C., Harris, I., Kruizinga, G., Romans, L., Watkins, M., Wu, S., 2003. Relative Time and Frequency Alignment Between Two Low Earth Orbiters, GRACE. Proc. IEEE Int. Frequency Control Syrup. and PDA Ex- hibition Jointly with the 17th European Frequency and Time Forum, p.273-279. [doi:10.1109/FREQ.2003. 1275101].
  • 4Dean, B., 2003. PLL Performance, Simulation and Design. National Semiconductor, p.88-150.
  • 5Kim, J., 2000. Simulation Study of a Low-Low Satellite-to- Satellite Tracking Mission. PhD Thesis, University of Texas at Austin, USA.
  • 6Kim, J., 2007. Measurement Time Synchronization for a Satellite-to-Satellite Ranging System. Proc. Int. Conf. Control, Automation and Systems, p. 190-194.
  • 7Kim, J., Tapley, B.D., 2002. Error analysis of a low-low satellite-to-satellite tracking mission. J. Guid. Control Dyn., 25(6):1100-1106. [doi:10.2514/2.4989].
  • 8Kim, J., Tapley, B.D., 2003. Simulation of dual one-way ranging measurements. J. Spacecraft Rockets, 40(3): 419-425. [doi:10.2514/2.3962].
  • 9Kim, J., Tapley, B.D., 2005. Optimal frequency configuration for dual one-way ranging systems. J. Spacecraft Rockets, 42(4):749-751. [doi:10.2514/1.9974].
  • 10Macarthur, J.L., Posner, A.S., 1985. Satellite-to-satellite range-rate measurement. 1EEE Trans. Geosci. Remote Sens., 23(4): 517-523. [doi:10.1109FI-GRS. 1985.289443].

共引文献1

同被引文献6

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