Skip to main content
Log in

Design and derivation of the dual transponder carrier ranging system

  • Published:
Journal of Zhejiang University SCIENCE C Aims and scope Submit manuscript

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.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  • 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.

    Google Scholar 

  • 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.

    Google Scholar 

  • 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. [doi:10.1109/FREQ.2003.1275101]

    Chapter  Google Scholar 

  • Dean, B., 2003. PLL Performance, Simulation and Design. National Semiconductor, p.88–150.

    Google Scholar 

  • Kim, J., 2000. Simulation Study of a Low-Low Satellite-to-Satellite Tracking Mission. PhD Thesis, University of Texas at Austin, USA.

    Google Scholar 

  • Kim, J., 2007. Measurement Time Synchronization for a Satellite-to-Satellite Ranging System. Proc. Int. Conf. Control, Automation and Systems, p.190–194.

    Google Scholar 

  • 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. [doi:10.2514/2.4989]

    Article  Google Scholar 

  • Kim, J., Tapley, B.D., 2003. Simulation of dual one-way ranging measurements. J. Spacecraft Rockets, 40(3): 419–425. [doi:10.2514/2.3962]

    Article  Google Scholar 

  • Kim, 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]

    Article  Google Scholar 

  • Macarthur, J.L., Posner, A.S., 1985. Satellite-to-satellite range-rate measurement. IEEE Trans. Geosci. Remote Sens., 23(4): 517–523. [doi:10.1109/TGRS.1985.289443]

    Article  Google Scholar 

  • Stephens, D., 2002. Phase-Locked Loops for Wireless Communications (2nd Ed.). Kluwer Academic Publishers, p.47–56, 353–400.

    Google Scholar 

  • Thomas, J.B., 1989. An Analysis of Digital Phase-Locked Loops. JPL Publication 89-2, Pasadena, CA.

    Google Scholar 

  • 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.

    Google Scholar 

  • 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).

    Google Scholar 

  • 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. [doi:10.1109/ISDEA.2010.171]

    Google Scholar 

  • 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. [doi:10.1631/jzus.A0820802]

    Article  MATH  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Chun-hui Wang.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Zhao, Mc., Wang, Ch. & Jin, Zh. Design and derivation of the dual transponder carrier ranging system. J. Zhejiang Univ. - Sci. C 14, 383–394 (2013). https://doi.org/10.1631/jzus.C1200266

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1631/jzus.C1200266

Key words

CLC number

Navigation