Abstract
Modern observational techniques using ground-based and space-based instrumentation have enabled the measurement of the distance between the instrument and satellite to better than one centimeter. Such high precision instrumentation has fostered applications with centimeter-level requirements for satellite position knowledge. The determination of the satellite position to such accuracy requires a comparable modeling of the forces experienced by the satellite, especially when classical orbit determination methods are used. Geodetic satellites, such as Lageos, in conjunction with high precision ground-based laser ranging, have been used to improve for modeling of forces experienced by the satellite. Space-based techniques, such as Global Positioning System (GPS), offer alternatives, including kinematic techniques which require no modeling of the satellite forces, or only rudimentary models. This paper will describe the various techniques and illustrate the accuracies achieved with current satellites, such as TOPEX/POSEIDON, GPS/MET and the expectations for some future satellites.
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References
Hoffmann-Wellenhof, B., Lichtenegger, H., and Collins, J.: 1993, GPS: Theory and Practice, Springer-Verlag, Wien and New York.
Lundberg, J.B.:1985, “Computational errors and their control in the determination of satellite orbits”, CSR-85-3, March 1985, Univ. of Texas at Austin, Center for Space Research.
Lundberg, J.B., Schutz, B.E., Fields, R., and Watkins, M.: 1991, “Application of Encke’s method to long arc orbit determination solutions”, J. Guid. Control Dyn. 14(3), 683–686.
McCarthy, D.:1996, “IERS Conventions (1996)”, IERS Tech. Note 21, Obs. de Paris.
Melbourne, W., Davis, E., Yunck, T., and Tapley, B.: 1994, “The GPS flight experiment on TOPEX/POSEIDON”, Geophys. Res. Lett. 21, 2171–2174.
Montenbruck, O.: 1992, “Numerical integration methods for orbital motion”, Celest. Mech. 53, 59–69.
Schutz, B.E. and Tapley, B.:1980, “Orbit determination and model improvement for Seasat and Lageos”, AIAA/AAS, Danvers, Paper 80-1679.
Schutz, B.E., Tapley, B., Abusali, P., and Rim, H.: 1994, “Dynamic orbit determination using GPS measurements from TOPEX/POSEIDON”, Geophys. Res. Lett. 21, 2179–2182.
Schutz, B. et al.: 1995, “GPS tracking experiment of a free-flyer deployed from Space Shuttle”, Proceedings of GPS-95, Institute of Navigation, 229-235.
Shampine, L. and Gordon, M.: 1975, Computer Solution of Ordinary Differential Equations: The Initial Value Problem, W. H. Freeman and Company, San Francisco.
Tapley, B., Schutz, B.E., Eanes, R., Ries, J., and Watkins, M.: 1993, “Lageos laser ranging contributions to geodynamics, geodesy and orbital dynamics”, Contributions of Space Geodesy to Geodynamics: Earth Dynamics (D. Smith, D. Turcotte, eds), American Geophysical Union 24, 147–174.
Yunck, T., et al.: 1994, “First assessment of GPS-based reduced dynamic orbit determination on TOPEX/POSEIDON”, Geophys. Res. Lett. 21, 541–544.
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© 1997 Springer Science+Business Media Dordrecht
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Schutz, B.E. (1997). New Observational Techniques and Precise Orbit Determination of Artificial Satellites. In: Wytrzyszczak, I.M., Lieske, J.H., Feldman, R.A. (eds) Dynamics and Astrometry of Natural and Artificial Celestial Bodies. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-5534-2_9
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DOI: https://doi.org/10.1007/978-94-011-5534-2_9
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