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A UT positioning approach for dynamic satellite constellationsIn this paper, we discuss a new positioning scheme which is thought to be applicable for dynamic satellite constellations. We begin with the introduction of our filter model which is based on stochastic process and filtering theory. Then, simulation results of the technique are presented based on a LEO constellation and some of the IRIDIUM system parameters. Performance of this algorithm is investigated under various noise conditions. Finally, several applications of this UT (user terminal) positioning algorithm are discussed.
Document ID
19960022459
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
Authors
Zhao, W. (Surrey Univ. Guildford, United Kingdom)
Tafazolli, R. (Surrey Univ. Guildford, United Kingdom)
Evans, B. G. (Surrey Univ. Guildford, United Kingdom)
Date Acquired
August 17, 2013
Publication Date
January 1, 1995
Publication Information
Publication: Proceedings of the Fourth International Mobile Satellite Conference (IMSC 1995)
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
96N25413
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19960022452Collected WorksProceedings of the Fourth International Mobile Satellite Conference (IMSC 1995)
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