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A new model for yaw attitude of Global Positioning System satellitesProper modeling of the Global Positioning System (GPS) satellite yaw attitude is important in high-precision applications. A new model for the GPS satellite yaw attitude is introduced that constitutes a significant improvement over the previously available model in terms of efficiency, flexibility, and portability. The model is described in detail, and implementation issues, including the proper estimation strategy, are addressed. The performance of the new model is analyzed, and an error budget is presented. This is the first self-contained description of the GPS yaw attitude model.
Document ID
19960009521
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bar-Sever, Y. E. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
November 15, 1995
Publication Information
Publication: The Telecommunications and Data Acquisition Progress Report 42-123
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
96N16687
Funding Number(s)
PROJECT: RTOP 314-30-11-50-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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