Abstract: | In this paper preliminary flight tests results are presented for a feasibility study of using differential GPS precision approach and landings augmented with pseudolites. Flight tests have been carried out by the DSO National Laboratories, Singapore, and the Satellite Navigation and Positioning (SNAP) group of the University of New South Wales. Trials were carried out in April/May 2003, at the Wedderburn Airfield, Australia, to assess the capabilities and limitations of an integrated differential GPS/pseudolite navigation system. The results of the tests indicate that carrier-smoothed code-phase differential GPS/pseudolite can satisfy vertical and lateral accuracies consistent with RNP for CAT III landing. |
Published in: |
Proceedings of the 16th International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GPS/GNSS 2003) September 9 - 12, 2003 Oregon Convention Center Portland, OR |
Pages: | 2318 - 2325 |
Cite this article: | Soon, B.K.H., Poh, E.K., Barnes, J., Zhang, J., Lee, H.K, Lee, H.K., Rizos, C., "Flight Test Results of Precision Approach and Landing Augmented by Airport Pseudolites," Proceedings of the 16th International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GPS/GNSS 2003), Portland, OR, September 2003, pp. 2318-2325. |
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