DocumentCode :
3033127
Title :
Analysis of a microsensor automatic gain control loop
Author :
M´Closkey, Robert T. ; Vakakis, Alex
Author_Institution :
Dept. of Mech. Aerosp. Eng., California Univ., Los Angeles, CA, USA
Volume :
5
fYear :
1999
fDate :
1999
Firstpage :
3307
Abstract :
We present the analysis of a nonlinear control system that is used to excite and maintain a specified amplitude of a lightly damped degree of freedom in the Jet Propulsion Laboratory microgyroscope. One- and two-degree-of-freedom models are considered. The analysis suggests that the perturbing effect of an additional weakly coupled degree of freedom does not quantitatively effect the operation of the automatic gain control
Keywords :
automatic gain control; control system analysis; gyroscopes; microsensors; nonlinear control systems; Jet Propulsion Laboratory microgyroscope; lightly damped degree of freedom; microsensor automatic gain control loop; nonlinear control system; one-degree-of-freedom model; perturbing effect; two-degree-of-freedom model; Aerospace engineering; Electrodes; Frequency; Gain control; Industrial engineering; Laboratories; Microsensors; Oscillators; Propulsion; Solid modeling;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1999. Proceedings of the 1999
Conference_Location :
San Diego, CA
ISSN :
0743-1619
Print_ISBN :
0-7803-4990-3
Type :
conf
DOI :
10.1109/ACC.1999.782377
Filename :
782377
Link To Document :
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