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.
Integrated inertial stellar attitude sensor
2007-05-08
Miscellaneous
No indication
English
Integrated Inertial Stellar Attitude Sensor
NTIS | 2003
|Performance Evaluation of a Stellar-Inertial Attitude Sensor Based on Particle Filtering AIAA Paper
British Library Conference Proceedings | 2007
|A method of stellar-inertial attitude determination under high dynamic condition
British Library Online Contents | 2014
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