Inherently robust micromachined gyroscopes with 2-DOF sense-mode oscillator

被引:85
作者
Acar, C [1 ]
Shkel, AM [1 ]
机构
[1] Univ Calif Irvine, Dept Mech & Aerosp Engn, Microsyst Lab, Irvine, CA 92697 USA
关键词
inertial sensor; MEMS gyroscope; micromachined gyroscope; rate sensor;
D O I
10.1109/JMEMS.2006.872224
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 [电气工程]; 0809 [电子科学与技术];
摘要
Commercialization of reliable vibratory micromachined gyroscopes for high-volume applications has proven to be extremely challenging, primarily due to the high sensitivity of the dynamical system response to fabrication and environmental variations. This paper reports a novel micromachined gyroscope with two degrees-of-freedom (DOF) sense-mode oscillator that provides inherent robustness against structural parameter variations. The 2-DOF sense-mode oscillator provides a frequency response with two resonant peaks and a flat region between the peaks, instead of a single resonance peak as in conventional gyroscopes. The device is nominally operated in the flat region of the sense-mode response curve, where the amplitude and phase of the response are insensitive to parameter fluctuations. Furthermore, the sensitivity is improved by utilizing dynamical amplification of oscillations in the 2-DOF sense-mode oscillator. Thus, improved robustness to variations in temperature, damping, and structural parameters is achieved, solely by the mechanical system design. Prototype gyroscopes were fabricated using a bulk-micromachining process, and the performance and robustness of the devices have been experimentally evaluated. With a 25 V dc bias and 3 V ac drive signal resulting in 5.8 pm drive-mode amplitude, the gyroscope exhibited a measured noise-floor of 0.64 degrees/s/root Hz over 50 Hz bandwidth in atmospheric pressure. The sense-mode response in the flat operating region was also experimentally demonstrated to be inherently insensitive to pressure, temperature, and dc bias variations.
引用
收藏
页码:380 / 387
页数:8
相关论文
共 14 条
[1]
Nonresonant micromachined gyroscopes with structural mode-decoupling [J].
Acar, C ;
Shkel, AM .
IEEE SENSORS JOURNAL, 2003, 3 (04) :497-506
[2]
ACAR C, 2005, NSTI NAN C AN CA, V3, P375
[3]
Acar C., 2004, THESIS U CALIFORNIA
[4]
CLARK WA, 1996, SOL STAT SENS ACT WO, P283
[5]
Parallel-plate electrostatic dual-mass oscillator [J].
Dyck, CW ;
Allen, JJ ;
Huber, RJ .
MICROMACHINED DEVICES AND COMPONENTS V, 1999, 3876 :198-209
[6]
GEIGER W, 2001, IEEE SENS J, P170
[7]
GREEN JA, 1998, SOL STAT SENS ACT WO, P51
[8]
Greiff P., 1991, TRANSDUCERS '91. 1991 International Conference on Solid-State Sensors and Actuators. Digest of Technical Papers (Cat. No.91CH2817-5), P966, DOI 10.1109/SENSOR.1991.149051
[9]
LELAND RP, 2001, P IEEE C DEC CONTR O
[10]
PARK S, 2001, AM CONTR C ARL VA JU