DocumentCode
2271121
Title
Tuning of MEMS Gyroscope using Evolutionary Algorithm and “ switched drive-angle ” method
Author
Keymeulen, D. ; Ferguson, M.I. ; Breuer, Lukas ; Peay, C. ; Oks, B. ; Yen-Cheng ; Kim, Dongkyu ; MacDonald, E. ; Foor, D. ; Terrile, R. ; Yee, K.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
fYear
2006
fDate
4-11 March 2006
Firstpage
1
Lastpage
8
Abstract
We propose a tuning method for micro-electro-mechanical systems (MEMS) gyroscopes based on evolutionary computation that has the capacity to efficiently increase the sensitivity of MEMS gyroscopes through tuning and, furthermore, to find the optimally tuned configuration for this state of increased sensitivity. We present the results of an experiment to determine the speed and efficiency of an evolutionary algorithm applied to electrostatic tuning of MEMS micro gyros. The MEMS gyro used in this experiment is a Pyrex post resonator gyro (PRG) in a closed-loop control system. A measure of the quality of tuning is given by the difference in resonant frequencies, or frequency split, for the two orthogonal rocking axes. The current implementation of the closed-loop platform is able to measure and attain a relative stability in the sub-millihertz range, leading to a reduction of the frequency split to less than 100 mHz
Keywords
circuit tuning; closed loop systems; evolutionary computation; gyroscopes; microsensors; MEMS gyroscope tuning; MEMS gyroscopes; MEMS micro gyros; PRG; Pyrex post resonator gyro; closed-loop control system; electrostatic tuning; evolutionary algorithm; evolutionary computation; microelectro-mechanical systems; switched drive-angle; Control systems; Current measurement; Electrostatic measurements; Evolutionary computation; Frequency measurement; Gyroscopes; Microelectromechanical systems; Micromechanical devices; Resonant frequency; Tuning;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2006 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-9545-X
Type
conf
DOI
10.1109/AERO.2006.1655973
Filename
1655973
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