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Integrated inertial stellar attitude sensor

Author
Wyman, Jr., William F.
Published
May 8, 2007.
Physical Description
1 electronic document
Additional Creators
Brady, Tye M. and Kourepenis, Anthony S.
Online Version

Availability

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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
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.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 20080009483.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 17027815