Abstract
Since the first demonstrations of airborne kinematic positioning using GPS carrier phase measurements in 1985, the ability to do practical and reliable kinematic GPS solutions in support of operational remote sensing activities has improved significantly. These improvemtns arise from a combination of factors including: GPS receivers able to track 8 or more satellites, more precise pseudorange measurements, the availability of post-processed precise satellite ephemerides, and the development of algorithms to initialize phase bias’s while in motion with a minimal amount of phase and pseudorange measurements. These factors have combined to produce an operational kinematic positioning capability accurate to centimeters while extending the range of the technique to hundreds of kilometers. The integer search algorithms used by KARS, that provide on-the-fly bias initialization and cycle slip fixing over extended range operations are described.
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References
Krabill, W.B., and Martin, C.F., Aircraft Positioning Using Global Positioning System Carrier Phase Data, Journal of the Institute of Navigation, Vol. 34, No. 1, 1987
Mader, G.L., Aircraft Positioning Using GPS Carrier Phase Measurements, Fall AGU Meeting, San Francisco, December 1985.
Mader, G.L., Dynamic Positioning Using GPS Carrier Phase Measurements, Manuscripta Geodaetica, 11, 1986.
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© 1996 Springer-Verlag Berlin Heidelberg
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Mader, G.L. (1996). Kinematic and Rapid Static (KARS) GPS Positioning: Techniques and Recent Experiences. In: Beutler, G., Melbourne, W.G., Hein, G.W., Seeber, G. (eds) GPS Trends in Precise Terrestrial, Airborne, and Spaceborne Applications. International Association of Geodesy Symposia, vol 115. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-80133-4_26
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DOI: https://doi.org/10.1007/978-3-642-80133-4_26
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-60872-1
Online ISBN: 978-3-642-80133-4
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