INTEGRATED INERTIAL STELLAR ATTITUDE SENSOR
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 respon...
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Main Authors | , , |
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Format | Patent |
Language | English |
Published |
02.02.2004
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Subjects | |
Online Access | Get full text |
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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. |
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Bibliography: | Application Number: AU20030247873 |