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Going Up. A GPS Receiver Adapts to SpaceCurrent plans for the space station call for the GPS receiver to be installed on the U.S. lab module of the station in early 2001 (ISS Assembly Flight SA), followed by the attachment of the antenna array in late 2001 (Flight 8A). At that point the U.S. ISS guidance and control system will be operational. The flight of SIGI on the space station represents a "coming of age" for GPS technology on spacecraft. For at least a decade, the promise of using GPS receivers to automate spacecraft operations, simplify satellite design, and reduce mission costs has enticed satellite designers. Integration of this technology onto spacecraft has been slower than some originally anticipated. However, given the complexity of the GPS sensor, and the importance of the functions it performs, its incorporation into mainstream satellite design has probably occurred at a very reasonable pace. Going from providing experimental payloads on small, unmanned satellites to performing critical operational functions on manned vehicles has been a major evolution. If all goes as planned in the next few months, GPS receivers will soon provide those critical functions on one of the most complex spacecraft in history, the International Space Station.
Document ID
20110001619
Acquisition Source
Johnson Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Lightsey, E. Glenn
(Texas Univ. Houston, TX, United States)
Simpson, James E.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 25, 2013
Publication Date
June 1, 2000
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
JSC-CN-6423
Report Number: JSC-CN-6423
Funding Number(s)
CONTRACT_GRANT: NAG9-1187
Distribution Limits
Public
Copyright
Public Use Permitted.
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