DocumentCode
1145108
Title
Development of a Low-Power Digital Inertial Reference Assembly
Author
Bicking, R.E.
Author_Institution
Honeywell Inc., Minneapolis, Minn.
Issue
3
fYear
1971
fDate
5/1/1971 12:00:00 AM
Firstpage
544
Lastpage
549
Abstract
Current and projected system requirements for inertial reference assemblies emphasize high accuracy, long life, and low power. An inertial reference assembly ( IRA) which embodies the aforementioned characteristics was developed recently. Pulse rebalanced gas-bearing gyroscopes were used to attain high accuracy and long life. Temperature compensation of gyroscope parameters (in lieu of temperature control) and dual voltage spinmotor operation helped achieve low-power operation. The latter two items represent an advancement in the state of the art and form the subject of this paper. These techniques were used in the construction of a three-axis IRA with an operating power less than 50 watts. It has achieved 0.1 percent scale factor accuracy over a 60°F range.
Keywords
Assembly; Costs; Damping; Equations; Gyroscopes; Space vehicles; Temperature control; Temperature distribution; Temperature sensors; Thermal resistance;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1971.310297
Filename
4103745
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