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Integrated inertial stellar attitude sensorAn integrated inertial stellar attitude sensor for an aerospace vehicle includes a star camera system, a gyroscope system, a controller system for synchronously integrating an output of said star camera system and an output of said gyroscope system into a stream of data, and a flight computer responsive to said stream of data for determining from the star camera system output and the gyroscope system output the attitude of the aerospace vehicle.
Document ID
20080009483
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - Patent
Authors
Brady, Tye M.
Kourepenis, Anthony S.
Wyman, Jr., William F.
Date Acquired
August 24, 2013
Publication Date
May 8, 2007
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-10/621,097
Patent Number: US-Patent-7,216,036
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,216,036
Patent Application
US-Patent-Appl-SN-10/621,097

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