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Comparison of GPS-Based Position Estimation Methods

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Solutions for Maintenance Repair and Overhaul (ISATECH 2021)

Part of the book series: Sustainable Aviation ((SA))

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Abstract

This chapter is devoted comparison of stationary user localization estimation by traditional extended Kalman filter (EKF), linear Kalman filter (LKF), and NRM pre-processed LKF. In this study, Şükrü Saraçoğlu stadium’s location was estimated via various types of Kalman filters. Position states due to Earth-centered inertial (ECI) reference frame were obtained by the Global Positioning System (GPS) receiver. Pseudo-ranging model was used to determining the position of Şükrü Saraçoğlu stadium. To simulate GPS receiver, random measurement errors were added to the actual distance between the stadium and GPS satellite. In this study, various filters were compared for stationary user localization estimation.

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References

  • Cheung, K., & Lee, C. (2017). A new geometric trilateration scheme for GPS-style localization. IPN Progress Report, pp. 42–209.

    Google Scholar 

  • Erkec, T. Y., & Hajiyev, C. (2019). Traditional methods on relative navigation of small satellites. In 2019 9th international conference on recent advances in space technologies (RAST), Istanbul, Turkey, pp. 869–874.

    Google Scholar 

  • Kumar, A., & Rao, G. S. (2019, May). Unscented kalman dilter for GPS based positioning and tracking services. International Journal of Innovative Technology and Exploring Engineering (IJITEE). (Vol. 8)

    Google Scholar 

  • Maldonado, A. L., Baylocq, M., & Hannan, G. (1984, June 25–27). Autonomous spacecraft navigation - extended Kalman filter estimation of classical orbital parameters. In 17th fluid dynamics, plasma dynamics, and lasers conference.

    Google Scholar 

  • Soken, H. E., & Hajiyev, C. (2010). Pico satellite attitude estimation via robust unscented Kalman filter in the presence of measurement faults. ISA Trans., 49, 249–256.

    Google Scholar 

  • Soken, H., & Hajiyev, C. (2012). Robust Estimation of UAV Dynamics in Presence of Measurements Faults. Journal of Aerospace Engineering. 25, 1–10. https://doi.org/10.1061/(ASCE)AS.1943-5525.0000095

  • Wertz, J. R. (1992, April 28). Autonomous spacecraft navigation system. United States Patent, Patent no:5109346.

    Google Scholar 

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Sever, M., Hajiyev, C. (2024). Comparison of GPS-Based Position Estimation Methods. In: Karakoc, T.H., Rohács, J., Rohács, D., Ekici, S., Dalkiran, A., Kale, U. (eds) Solutions for Maintenance Repair and Overhaul. ISATECH 2021. Sustainable Aviation. Springer, Cham. https://doi.org/10.1007/978-3-031-38446-2_54

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  • DOI: https://doi.org/10.1007/978-3-031-38446-2_54

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-031-38445-5

  • Online ISBN: 978-3-031-38446-2

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