Skip to main content
Log in

Effect of PDOP on performance of Kalman Filters for GNSS-based space vehicle position estimation

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

Abstract

A theoretical performance analysis of Kalman Filters for Global Navigation Satellite System GNSS-based space vehicle position estimation in varying Position Dilution of Precision (PDOP) conditions is presented. The PDOP indicates the possible accuracy of GNSS measurements using Least Square Estimation (LSE). The Kalman Filter combines the knowledge of the vehicle motion with the GNSS measurements and then provides better accuracy than the LSE. For the same nonlinear vehicular motion and PDOP condition, the ratio of average position error and noise standard deviation varies depending on the type of Kalman Filter used. The presented theoretical analysis explains and characterizes this behavior for four Kalman Filters, which are the Extended Kalman Filter (EKF), the Unscented Kalman Filter (UKF) and two newly developed Unscented Type Kalman Filters. The experiment shows that for highly nonlinear space vehicle motion, the performance of the UKF is better than the EKF in high PDOP conditions and all the filters perform similarly for low PDOP conditions. For a space vehicle with lower nonlinearity in the motion, the performances of all the filters are indistinguishable for any PDOP condition.

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.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11

Similar content being viewed by others

References

  • Bar-shalom Y, Li X, Kirubarajan T (2004) Estimation with applications to tracking and navigation: theory algorithms and software. Wiley, New York

    Google Scholar 

  • Biswas SK, Qiao L, Dempster A (2015) Application of a fast unscented Kalman Filtering method to satellite position estimation using a space-borne multi-GNSS receiver. In: Proceedings of ION GNSS+ 2016, Institute of Navigation, Tampa, Florida, September 2015, pp 2625–2631

  • Biswas SK, Qiao L, Dempster AG (2016a) A novel a priori state computation strategy for the unscented Kalman filter to improve computational efficiency. IEEE Trans Autom Control. doi:10.1109/TAC.2016.2599291

    Google Scholar 

  • Biswas SK, Qiao L, Dempster AG (2016b) Computationally efficient unscented Kalman Filtering techniques for launch vehicle navigation using a space-borne GPS receiver. In: Proceedings of ION GNSS+ 2016, Institute of Navigation, Portland, Oregon, September 2016, pp 186–194

  • Braun B, Markgraf M, Montenbruck O (2016) Performance analysis of IMU-augmented GNSS tracking systems for space launch vehicles. Ceas Space J 8:117. doi:10.1007/s12567-016-0113-9

    Article  Google Scholar 

  • Choi EJ, Yoon JC, Lee BS, Park SY, Choi KH (2010) Onboard orbit determination using GPS observations based on the unscented Kalman filter. Adv Space Res 46(11):1440–1450

    Article  Google Scholar 

  • Curtis HD (2010) Orbital mechanics for engineering students. Butterworth-Heinemann, Oxford

    Google Scholar 

  • Doong SH (2009) A closed-form formula for GPS GDOP computation. GPS Solut 13(3):183–190

    Article  Google Scholar 

  • Julier S, Uhlmann J (1997). A new extension of the Kalman filter to nonlinear systems. In: Proceedings of signal processing, sensor fusion, and target recognition VI, Orlando, Florida, April 1997, pp 182–193

  • Julier SJ, Uhlmann JK (2004) Unscented filtering and nonlinear estimation. Proc IEEE 92(3):401–422

    Article  Google Scholar 

  • Julier S, Uhlmann J, Durrant-Whyte HF (2000) A new method for the nonlinear transformation of means and covariances in filters and estimators. IEEE Trans Autom Control 45(3):477–482

    Article  Google Scholar 

  • Kalman RE (1960) A new approach to linear filtering and prediction problems. Trans ASME J Basic Eng 82((Series D)):35–45

    Article  Google Scholar 

  • Kaplan ED, Hegarty CJ (eds) (2005) Understanding GPS: principles and applications. In: Understanding GPS: principles and applications. Artech house, Boston

  • Misra P, Enge P (2006) Global positioning system: signals, measurements and performance. Ganga-Jamuna Press, Lincoln

    Google Scholar 

  • Montenbruck O, Gill E (2012) Satellite orbits: models, methods and applications. Springer, Berlin

    Google Scholar 

  • Montenbruck O, Ramos-Bosch P (2008) Precision real-time navigation of LEO satellites using global positioning system measurements. GPS Solut 12(3):187–198

    Article  Google Scholar 

  • Montenbruck O, Hauschild A, Andres Y, Engeln A, Marquardt C (2012) (Near-)real-time orbit determination for GNSS radio occultation processing. GPS Solut 17(2):199–209

    Article  Google Scholar 

  • Nadarajah N, Teunissen PJG, Buist PJ (2012) Attitude determination of LEO satellites using an array of GNSS sensors. In: Proceedings of 15th international conference on information fusion (FUSION), Singapore 2012, pp 1066–1072

  • NASA (2014) SpaceX CRS-5 fifth commercial resupply services flight to the international space station

  • Parkinson KJ, Mumford PJ, Glennon EP, Shivaramaiah NC, Dempster AG, Rizos C (2011) A low cost Namuru V3 receiver for Spacecraft operations. In: Proceedings of IGNSS symposium 2011, pp 15–17

  • Qiao L, Samsung L, Rizos C (2009) A multiple GNSS-based orbit determination algorithm for geostationary satellites. In: Proceedings of IGNSS symposium 2009

  • SpaceX (2009). Falcon 9 launch vehicle payload user’s guide revision 1

  • Vallado DA (2001) Fundamentals of astrodynamics and applications. Springer, Berlin

    Google Scholar 

  • Yunck TP (1993) Coping with the atmosphere and ionosphere in precise satellite and ground positioning. Washington DC American Geophysical Union Geophysical Monograph Series, 73, pp 1–16

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Sanat K. Biswas.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Biswas, S.K., Qiao, L. & Dempster, A.G. Effect of PDOP on performance of Kalman Filters for GNSS-based space vehicle position estimation. GPS Solut 21, 1379–1387 (2017). https://doi.org/10.1007/s10291-017-0621-x

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10291-017-0621-x

Keywords

Navigation