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Vol: 57(71) No: 1 / March 2012      

Closed Loop High-Precision Accelerometer with Smart Control
T. L. Grigorie
Avionics Division, University of Craiova, Faculty of Electrical Engineering, 107 Decebal Blvd., 200440 Craiova, Romania, phone: (+40) 251-436447, e-mail: lgrigore@elth.ucv.ro
M. Lungu
Avionics Division, University of Craiova, Faculty of Electrical Engineering, 107 Decebal Blvd., 200440 Craiova, Romania, e-mail: mlungu@elth.ucv.ro
I. R. Edu
Avionics Division, University of Craiova, Faculty of Electrical Engineering, 107 Decebal Blvd., 200440 Craiova, Romania, e-mail: edu_ioana_raluca@yahoo.com
R. Obreja
Avionics Division, University of Craiova, Faculty of Electrical Engineering, 107 Decebal Blvd., 200440 Craiova, Romania, e-mail: radu@sistemeuroteh.ro


Keywords: accelerometer, precision improvement, closed-loop, control, fuzzy logic

Abstract
The paper presents a way to improve the transient regime of a miniature accelerometer by using a smart controller to close its loop. Firstly, the classical architecture of the accelerometer is derived, and the optimal numerical values for its parameters are estimated. The smart controller is a fuzzy controller and replaces an electronic block on the feedback path of the closed loop, block that, in the classical architecture, assured the system damping and, in the same time, played the role of elastic link of the accelerometer proof mass. For the proposed controller, proportional-derivative variant is chosen, and its input-output mapping is derived. The membership functions for inputs are s-functions, π-functions, respectively z-functions, while the output membership functions have constant values. To define the rules, a zero-order Sugeno fuzzy model is chosen. Finally, a comparative numerical study between the classical and the proposed accelerometer architectures is made.

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