DocumentCode
789725
Title
Stability of a two-degree-of-freedom gyro with external feedback
Author
Briggs, R.W.
Author_Institution
Hughes Aircraft Company, Culver City, CA, USA
Volume
10
Issue
3
fYear
1965
fDate
7/1/1965 12:00:00 AM
Firstpage
244
Lastpage
249
Abstract
The requirements for insuring the stability of the loop formed when external feedback is applied to a two-degree-of-freedom gyro are determined. The method of analysis also suggests the means for increasing the damping of the nutation of a precessible two-degree-of-freedom gyro when it is used in a free mode.
Keywords
Gyroscopes; Stability; Construction; Damping; Feedback loop; Laplace equations; Missiles; Radar antennas; Radar tracking; Sensor systems; Stability; Torque;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.1965.1098157
Filename
1098157
Link To Document