Skip to main content
Log in

Ultra-tight GPS/INS/PL integration: a system concept and performance analysis

  • Review Article
  • Published:
GPS Solutions Aims and scope Submit manuscript

Abstract

The architecture of the ultra-tight GPS/INS/PL integration is the key to its successful performance; the main feature of this architecture is the Doppler feedback to the GPS receiver tracking loops. This Doppler derived from INS, when integrated with the carrier tracking loops, removes the Doppler due to vehicle dynamics from the GPS/PL signal thereby achieving a significant reduction in the carrier tracking loop bandwidth. The bandwidth reduction provides several advantages such as: improvement in anti-jamming performance, and increase in post correlated signal strength which in turn increases the dynamic range and accuracy of measurements. Therefore, any degradation in the derived Doppler estimates will directly affect the tracking loop bandwidth and hence its performance. The quadrature signals from the receiver correlator, I (in-phase) and Q (quadrature), form the measurements, whereas the inertial sensor errors, position, velocity and attitude errors form the states of the complementary Kalman filter. To specify a reliable measurement model of the filter for this type of integrated system, a good understanding of GPS/PL signal characteristics is essential. It is shown in this paper that phase and frequency errors are the variables that relate the measurements and the states in the Kalman filter. The main focus of this paper is to establish the fundamental mathematical relationships that form the measurement model, and to show explicitly how the system error states are related to the GPS/PL signals. The derived mathematical relationships encapsulated in a Kalman filter, are tested by simulation and shown to be valid.

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.

Institutional subscriptions

Fig. 1
Fig. 2
Fig. 3
Fig. 4

Similar content being viewed by others

References

  • Abbott S, Lillo WE (2003) Global Positioning System Inertial Measurement using Ultratight coupling method, US Patent # 6,516,021

  • Babu R, Wang J (2005) Analysis of INS-derived Doppler effects on carrier tracking loop. J Navig 58(3):493–507. doi:10.1017/S0373463305003309

    Article  Google Scholar 

  • Barnes J, Rizos C, Kanli M, Small D, Voigt G, Gambale N, Lamance J, Nunan T, Reid C (2004) Indoor industrial machine guidance using Locata: a pilot study at BlueScope Steel. In: 60th annual meeting of the US Institute of Navigation, Dayton, Ohio, 7–9 June, pp 533–540

  • Bar-Itzhack IY, Berman N (1988) Control theoretic approach to inertial navigation systems. AIAA J Guid Control Dyn 11:237–245. doi:10.2514/3.20299

    Article  Google Scholar 

  • Beser J, Alexander S, Crane R, Rounds S, Wyman J, Baeder B (2002) Trunav™: a low-cost guidance/navigation unit integrating a SAASM-based GPS and MEMS IMU in a deeply coupled mechanization. In: 15th International technical meeting of the satellite division of the US Institute of Navigation, Portland, 24–27 September, pp 545–555

  • Cahn RC, Leimer DK, Marsh CL, Huntowski FJ, Larue GD (1977) Software implementation of a PN spread spectrum receiver to accommodate dynamics. IEEE Trans Commun 25(8):832–839. doi:10.1109/TCOM.1977.1093904

    Article  Google Scholar 

  • Gustafson D, Dowdle J (2003) Deeply integrated code tracking: comparative performance analysis. In: 16th International technical meeting of the satellite division of the US Institute of Navigation, Portland, 9–12 September, pp 2553–2561

  • Jee GI et al (2002) A GPS C/A code tracking loop based on extended kalman filter with multipath mitigation. In: 15th International technical meeting of the satellite division of the US Institute of Navigation, Portland, 24–27 September, pp 446–451

  • Jwo D-J (2001) Optimization and sensitivity analysis of GPS receiver tracking loops in dynamic environments. IEE Proc Radar Sonar Navig 148:241–250. doi:10.1049/ip-rsn:20010429

    Article  Google Scholar 

  • Kee C, Yun D, Jun H, Parkinson B, Pullen S, Lagenstein T (2001) Centimeter-accuracy indoor navigation using GPS-like pseudolites. GPS World 12(11):14–22

    Google Scholar 

  • Lee HK, Wang J, Rizos C, Grejner-Brzezinska D (2004) Analyzing the impact of integrating Pseudolite observations into a GPS/INS system. J Surv Eng 130(2):95–103. doi:10.1061/(ASCE)0733-9453(2004)130:2(95)

    Article  Google Scholar 

  • Lee HK, Wang J, Rizos C (2005) An integer ambiguity resolution procedure for GPS/Pseudolite/INS integration. J Geod 79:242–255. doi:10.1007/s00190-005-0466-x

    Article  Google Scholar 

  • Maybeck PS (1979) Stochastic models, estimation, and control, volume I. Academic Press, New York

    Google Scholar 

  • Ohlmeyer EJ (2006) Analysis of an ultra-tightly coupled GPS/INS system in jamming. IEEE 44–53

  • Sennott JW, Senffner D (1992) The use of satellite geometry for prevention of cycle slips in a GPS processor. Navig J Inst Navig 39:217–235

    Google Scholar 

  • Sennott J, Senffner D (1997) Robustness of tightly coupled integrations for real-time centimeter GPS positioning. In: 10th International technical meeting of the satellite division of the US institute of navigation, Kansas City, 16–19 September, pp 655–663

  • Spilker (1996) Fundamentals of signal tracking theory. In: Global positioning system: theory and applications, Chap. 7. AIAA

  • Wang J, Dai L, Tsuiji T, Rizos C, Grejner-Brzezinska D, Toth C (2001) GPS/INS/Pseudolite integration: concepts, simulation and testing. In: 14th International technical meeting of the satellite division of the US Institte of Navigation, Salt Lake City, 11–14 September, pp 2708–2715

  • Wang J (2002) Pseudolite applications in positioning and navigation: progress and problems. J Glob Positioning Syst 1:48–56

    Google Scholar 

  • Ward P (1998) Performance comparisons between FLL, PLL and a novel FLL-assisted PLL carrier tracking loop under RF interference conditions. In: 11th International technical meeting of the satellite division of the US Institute of Navigation, Nashville, 15–18 September, pp 783–795

  • Wong RVC (1988) Development of a RLG strapdown inertial navigation system, PhD Thesis, USCE Report Number 20027, Department of Geomatics Engineering, The University of Calgary

  • Van DAJ, Fenton P, Ford T (1992) Theory and performance of narrow correlator spacing in a GPS receiver. Navig J Inst Navig 39:265–283

    Google Scholar 

  • Yun D, Kee C (2002) Centimeter accuracy stand-alone indoor navigation system by synchronized Pseudolite constellation. In: 15th International technical meeting of the satellite division of the US Institute of Navigation, Portland, 24–27 September, pp 213–225

Download references

Acknowledgments

This research is supported by an ARC (Australian Research Council)—Discovery Research Project on ‘Robust Positioning Based on Ultra-tight Integration of GPS, Pseudolites and Inertial Sensors’. The authors would like to thank the Editor-in-Chief Professor Alfred Leick, and the reviewers Dr. Mark Petovello and Dr. Alexey Zhdanov for their valuable comments on the previous versions of this paper.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Ravindra Babu.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Babu, R., Wang, J. Ultra-tight GPS/INS/PL integration: a system concept and performance analysis. GPS Solut 13, 75–82 (2009). https://doi.org/10.1007/s10291-008-0097-9

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10291-008-0097-9

Keywords

Navigation