NASA NTRS · 20080009483
Integrated inertial stellar attitude sensor
Abstract
An 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.
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Brady, Tye M., Kourepenis, Anthony S., Wyman, Jr., William F.. 2007-05-08. Integrated inertial stellar attitude sensor. https://ntrs.nasa.gov/citations/20080009483
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