Effects of Pseudolite Positioning on DOP in LAAS

Abstract

In this paper, effects on DOP (Dilution of Precision) due to augmentation of Global Positioning System (GPS) with pseudolites are investigated. For this purpose, a typical Local Area Augmentation System (LAAS) scenario is consi-dered by placing pseudolites in various positions. It is found that only properly located pseudolites can improve the DOP. DOP values with two pseudolites located on either side of the run way are found to be the best. Geometric DOP (max) was found to be nearly 4 due to only GPS and came down to approximately 2 due to augmentation with two pseudolites. Implementation aspects of Bayes and Kalman filters while estimating DOP values are also examined.

Share and Cite:

Q. Sultana, D. Sunehra, V. Srinivas and A. Sarma, "Effects of Pseudolite Positioning on DOP in LAAS," Positioning, Vol. 1 No. 1, 2010, pp. 18-26. doi: 10.4236/pos.2010.11003.

Conflicts of Interest

The authors declare no conflicts of interest.

References

[1] B. D. Elrod and A. J. Van Dierendonck, “Pseudolites,” In: B. W. Parkinson and J. J. Spilker, Ed., Global Positioning System: Theory and Applications (Vol. 2), American Institute of Astronautics, Washington D.C., 1996, pp. 51- 79.
[2] R. L. Harrington and J. T. Dolloff, “The Inverted Range: GPS User Test Facility,” IEEE PLANS’76, San Diego, California, 1-2 November 1976, pp. 204-211.
[3] E. Lemaster and S. Rock, “Mars Exploration Using Self-Calibrating Pseudolite Arrays,” 12th International Technical Meeting of the Satellite Division of the Institute of Navigation GPS-99, Nashville, Tennessee, 14-17 September 1999, pp. 1549-1558.
[4] “FAA Approves 1st U.S. Ground Based Augmentation System,” U.S. Federal Aviation Administration Washington Headquarters Press Release, 21 September, 2009.
[5] K. Zimmerman, “Experiments in the Use of the Global Positioning System for Space Vehicle Rendezvous,” Ph.D. Thesis, Stanford University, California, 1996.
[6] “Minimum Operational Performance Standards for GPS Local Area Augmentation System Airborne Equipment,” Washington D.C., RTCA SC-159, WG-4, DO-253C, 16 December, 2008.
[7] S. Bancroft, “An Algebraic Solution of the GPS Equations,” IEEE Transactions on Aerospace & Electronics Systems, Vol. 27, No. 6, 1985, pp. 56-59.
[8] K. Borre, “GPS MATLAB Tools at Aalborg University by Kai Borre,” May 2010.
[9] http://kom.aau.dk/~borre/matlab/-2k
[10] K. Borre and G. Strang, “Linear Algebra Geodesy and GPS,” Wellesley-Cambridge Press, USA, 1997.
[11] R. G. Brown and P. Y. C. Hwang, “GPS Failure Detection by Autonomous Means Within the Cockpit,” Proceedings of the Annual Meeting of the Institute of Navigation, Seattle, WA, 24-26 June 1986, pp. 5-12.
[12] P. Misra and P. Enge, “Global Positioning System-Sig- nals, Measurements and Performance,” Ganga-Jamuna Press, Lincoln, Massachusetts, USA, 2001.
[13] C. G. Bartone, and S. Kiran, “Flight Test Results of an Integrated Wideband Airport Pseudolite for the Local Area Augmentation System,” ION-GPS, Salt Lake City, Utah, 2000.
[14] C. E. Cohen, B. S. Pervan, H. S. Cobb, D. G. Lawrence, J. D. Powell and B. W. Parkinson, “Real-Time Cycle Ambiguity Resolution Using a Pseudolite for Precision Landing of Aircraft with GPS,” DSNS ’93, Amsterdam, The Netherlands, 30 March-2 April 1993, pp. 171-178.
[15] S. Fukushima, T. Yoshihara and S. Suga, “Evaluation of a Tropospheric Correction Model for Airport Pseudolite,” 17th International Technical Meeting of the Satellite Division of the Institute of Navigation, Long Beach, CA, 21-24 September 2004, pp. 2283-2288.
[16] W. B. Parkinson and J. J. Spilker, “Global Positioning System: Theory and Applications: Vol. 1 and 2,” American Institute of Aeronautics and Astronautics, Inc, Washington, 1996.

Copyright © 2024 by authors and Scientific Research Publishing Inc.

Creative Commons License

This work and the related PDF file are licensed under a Creative Commons Attribution 4.0 International License.