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Integrated inertial stellar attitude sensor
- Publication Year :
- 2007
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 2007.
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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.
- Subjects :
- Space Communications, Spacecraft Communications, Command And Tracking
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Publication Type :
- Report
- Accession number :
- edsnas.20080009483
- Document Type :
- Report