DocumentCode
979868
Title
Inertial-Guidance Limitations Imposed by Fluctuation Phenomena in Gyroscopes
Author
Newton, George C., Jr.
Author_Institution
Electronic Systems Lab., Dept. of Elec. Engrg., Massachtusetts Inistitute of Technology, Cambridge, Mass.
Volume
48
Issue
4
fYear
1960
fDate
4/1/1960 12:00:00 AM
Firstpage
520
Lastpage
527
Abstract
Because of recent improvements, inertial guidance is becoming increasingly important to space and missile programs in connection with the navigation of mobile bases and the launching of vehicles. Gyroscopes are an important component of inertial systems. In order to see if much room remains for further improvement, the performance limitation imposed by thermal fluctuations in gyroscopes is examined. This is done because experience in electronics shows that thermal noise is the ultimate performance limitation in sensitive instruments such as radio receivers and galvanometers. It is found that a system limited only by thermal noise in its gyroscopes would have several orders of magnitude more precision than that indicated in published performance data. This must mean that other factors are limiting performance of gyroscopes, and investigation of several of these shows that bearing noise may be an important one. In conclusion, since gyroscopes do not yet come near to attaining the performance limits set by thermal noise, there may be much room left for their further improvement.
Keywords
Acceleration; Aircraft navigation; Earth; Fluctuations; Gravity; Gyroscopes; Missiles; Space technology; Space vehicles; Underwater vehicles;
fLanguage
English
Journal_Title
Proceedings of the IRE
Publisher
ieee
ISSN
0096-8390
Type
jour
DOI
10.1109/JRPROC.1960.287401
Filename
4066050
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