CLC number: TN927
On-line Access: 2013-04-30
Received: 2012-09-17
Revision Accepted: 2013-02-27
Crosschecked: 2013-04-17
Cited: 1
Clicked: 8023
Ming-chen Zhao, Chun-hui Wang, Zhong-he Jin. Design and derivation of the dual transponder carrier ranging system[J]. Journal of Zhejiang University Science C, 2013, 14(5): 383-394.
@article{title="Design and derivation of the dual transponder carrier ranging system",
author="Ming-chen Zhao, Chun-hui Wang, Zhong-he Jin",
journal="Journal of Zhejiang University Science C",
volume="14",
number="5",
pages="383-394",
year="2013",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.C1200266"
}
%0 Journal Article
%T Design and derivation of the dual transponder carrier ranging system
%A Ming-chen Zhao
%A Chun-hui Wang
%A Zhong-he Jin
%J Journal of Zhejiang University SCIENCE C
%V 14
%N 5
%P 383-394
%@ 1869-1951
%D 2013
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.C1200266
TY - JOUR
T1 - Design and derivation of the dual transponder carrier ranging system
A1 - Ming-chen Zhao
A1 - Chun-hui Wang
A1 - Zhong-he Jin
J0 - Journal of Zhejiang University Science C
VL - 14
IS - 5
SP - 383
EP - 394
%@ 1869-1951
Y1 - 2013
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.C1200266
Abstract: The accuracy of microwave ranging is mainly limited by the frequency instability of the oscillator that generates the carrier phase signal. A dual transponder carrier ranging method is used to minimize the oscillator noise by combining the reference and the to-and-fro measurements. This ranging approach together with pseudo-noise ranging or other means can be used to measure the inter-satellite distance with a high precision. The pseudo-noise ranging system or other ranging systems help to solve the integer circles while the dual transponder ranging system guarantees the accurate fractional circle. The two satellites work in the master-slave mode. The range measurements are derived on the master satellite while the slave satellite just coherently transfers the received signal, so that the dual transponder ranging system does not need to rely on the time tagging system to synchronize the two satellites. This study first describes the dual transponder carrier ranging system and shows how the system removes most of the oscillator noise components effectively. Then, a detailed design scheme on the frequency planning of the ranging system is presented and the supporting analysis illustrates the feasibility of this system. Based on the design innovation, a laboratory demonstration system is assembled to verify the realizability of the dual transponder ranging system. The experimental results demonstrate that a high level of accuracy (about 30 μm under laboratory circumstance) can be achieved by the use of the proposed dual transponder carrier ranging system.
[1]Aguirre, 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.
[2]Bertiger, W., Bar-Sever, Y., Desai, S., Dunn, C., 2002. GRACE: Millimeters and Microns in Orbit. Proc. ION GPS, Institute of Navigation, p.2022-2029.
[3]Bertiger, 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 Symp. and PDA Exhibition Jointly with the 17th European Frequency and Time Forum, p.273-279.
[4]Dean, B., 2003. PLL Performance, Simulation and Design. National Semiconductor, p.88-150.
[5]Kim, J., 2000. Simulation Study of a Low-Low Satellite-to-Satellite Tracking Mission. PhD Thesis, University of Texas at Austin, USA.
[6]Kim, J., 2007. Measurement Time Synchronization for a Satellite-to-Satellite Ranging System. Proc. Int. Conf. Control, Automation and Systems, p.190-194.
[7]Kim, J., Tapley, B.D., 2002. Error analysis of a low-low satellite-to-satellite tracking mission. J. Guid. Control Dyn., 25(6):1100-1106.
[8]Kim, J., Tapley, B.D., 2003. Simulation of dual one-way ranging measurements. J. Spacecraft Rockets, 40(3):419-425.
[9]Kim, J., Tapley, B.D., 2005. Optimal frequency configuration for dual one-way ranging systems. J. Spacecraft Rockets, 42(4):749-751.
[10]Macarthur, J.L., Posner, A.S., 1985. Satellite-to-satellite range-rate measurement. IEEE Trans. Geosci. Remote Sens., 23(4):517-523.
[11]Stephens, D., 2002. Phase-Locked Loops for Wireless Communications (2nd Ed.). Kluwer Academic Publishers, p.47-56, 353-400.
[12]Thomas, J.B., 1989. An Analysis of Digital Phase-Locked Loops. JPL Publication 89-2, Pasadena, CA.
[13]Thomas, J.B., 1999. An Analysis of Gravity-Field Estimation Based on Inter-Satellite Dual-1-Way Biased Ranging. JPL Publication 98-15, Pasadena, CA.
[14]Wang, C.H., Yu, F.X., Jin, Z.H., Zheng, Y.M., Zhao, X.Y., 2006. Research on noise of TT&C transponder for pico-satellites. Syst. Eng. Electr., 28(12):1514-1517 (in Chinese).
[15]Yang, J., Yang, Y.K., Liang, L.F., Liu, L., 2010. Research on Digital Phase-Locked Loop about K/Ka-Band High Precision Receiver. Proc. Int. Intelligent System Design and Engineering Application Conf., p.185-188.
[16]Zhao, X.Y., Jin, X.J., Jin, Z.H., 2009. Simulation of dual transponder carrier ranging measurements. J. Zhejiang Univ.-Sci A, 10(10):1395-1403.
Open peer comments: Debate/Discuss/Question/Opinion
<1>