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Global Positioning System Satellite Selection MethodThe satellite selection method as utilized by the spaceborne Global Positioning System receiver provides navigational solutions and is designed for use in low Earth orbit. The satellite selection method is a robust algorithm that can be used a GPS receiver to select appropriate GPS satellites for use in calculating point solutions or attitude solutions. The method is takes into account the difficulty of finding a particular GPS satellite phase code, especially when the search range in greatly increased due to Doppler shifts introduced into the carrier frequency. The method starts with an update of the antenna pointing and spacecraft vectors to determine the antenna backplane direction. Next, the GPS satellites that will potentially be in view of the antenna are ranked on a list, whereby the list is generated based on the estimated attitude and position of each GPS satellite. Satellites blocked by the Earth are not entered on this list. A second list is created, whereby the GPS satellites are ranked according to their desirability for use in attitude determination. GPS satellites are ranked according to their orthogonality to the antenna backplane, and according to geometric dilution of precision considerations. After the lists are created, the channels of the spaceborne GPS receiver are assigned to various GPS satellites for acquisition and lock. Preliminary Doppler frequencies for searching are assigned to the various channels.
Document ID
20010110772
Acquisition Source
Goddard Space Flight Center
Document Type
Other - Patent
External Source(s)
GSC-13991-2
Authors
Frederick A Niles
(Goddard Space Flight Center Greenbelt, United States)
Date Acquired
August 20, 2013
Publication Date
August 21, 2001
Publication Information
Publisher: United States Patent and Trademark Office
Subject Category
Aircraft Communications And Navigation
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-6,278,404
Patent Application
US-Patent-Appl-SN-348875|US-Patent-Appl-SN-092491
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