DocumentCode
861192
Title
Analysis of gyro orientation
Author
Mayer, Arthur
Author_Institution
Reeves Instrument Corporation, Garden City, NY, USA
Volume
6
Issue
1
fYear
1958
fDate
12/1/1958 12:00:00 AM
Firstpage
93
Lastpage
101
Abstract
The frequency response of a gyro-stabilized platform is limited by the gyros. For the most effective suppression of instability with a minimum sacrifice in bandwidth, it is necessary to orient single-degree-of-freedom gyros in a certain way. Methods of orientation are discussed in this paper.
Keywords
Aircraft; Assembly; Bandwidth; Cities and towns; Frequency response; Instruments; Servomechanisms; Signal generators; Stability; Vehicles;
fLanguage
English
Journal_Title
Automatic Control, IRE Transactions on
Publisher
ieee
ISSN
0096-199X
Type
jour
DOI
10.1109/TAC.1958.1105170
Filename
1105170
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