2020
DOI: 10.1109/access.2020.2977223
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Design and Experiment for Dual-Mass MEMS Gyroscope Sensing Closed-Loop System

Abstract: A closed-loop controlling system for Micro Electro Mechanical System (MEMS) gyroscope sense mode is investigated in this paper, and the controller is designed to achieve low error, wide bandwidth and low noise capability. The gyroscope monitoring system includes four independent closed-loop, and is simulated by Simulink soft to prove the speedability and stability of the sensing closed-loop. The gyroscope monitoring system is realized through 3 analog circuit boards, and is tested through temperature controlle… Show more

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Cited by 30 publications
(19 citation statements)
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“…There are related simulations of the first four sequential modes in Ansys soft, as shown in Figure 2. In practice, the drive mode shows purely anti-phase mode drive, it is for three main reasons: the relevant excitation mode of the drive mode, the quality factor Rx2 of the anti-phase drive mode is greater than 2000, the frequency difference between the anti-phase mode and the in phase mode is more than 1000Hz., Since the actual sensing mode used for work consists of the second and the third mode, the motion equation of gyroscope structure can be expressed by Equation (1) in ideal case: (1) where, S = [x,y1,y2] T is the displacement, m = [mx,my,my] T is the mass, = [ , , ]…”
Section: Gyro Structurementioning
confidence: 99%
See 1 more Smart Citation
“…There are related simulations of the first four sequential modes in Ansys soft, as shown in Figure 2. In practice, the drive mode shows purely anti-phase mode drive, it is for three main reasons: the relevant excitation mode of the drive mode, the quality factor Rx2 of the anti-phase drive mode is greater than 2000, the frequency difference between the anti-phase mode and the in phase mode is more than 1000Hz., Since the actual sensing mode used for work consists of the second and the third mode, the motion equation of gyroscope structure can be expressed by Equation (1) in ideal case: (1) where, S = [x,y1,y2] T is the displacement, m = [mx,my,my] T is the mass, = [ , , ]…”
Section: Gyro Structurementioning
confidence: 99%
“…The MEMS gyroscope based on Coriolis acceleration mainly conveys vibration between the drive mode and the detection mode [1,2], due to its advantages such as robustness, low noise, and low power consumption [3], MEMS technology and gyroscopes have been widely used in aviation, aerospace, measuring and other important fields [4][5][6][7][8][9][10].…”
Section: Introductionmentioning
confidence: 99%
“…and using (11) in (10) yields (17). In order to avoid the random loss of measurement in calculating the Kalman gain K which introduces more errors, the first moments instead of measurements is used to determine the Kalman gain.…”
Section: ) Variational Bayesian Measurement Updatementioning
confidence: 99%
“…▪ Initialization by using (13) ▪ Update the state vector by using (15)- (17) ▪ Update the scale matrices (…”
Section: Variational Bayesian Measurement Updatementioning
confidence: 99%
“…The right and left sense frame movement signals were detected with the differential detection amplifier, while a second differential amplifier processed the output signal, in order to generate the sensing mode movement signal V stotal . To acquire the sense mode movement signal, V stotal was demodulated by V dac Sin(w d t) and, then, a low-pass filter was configured to eliminate the noise [28].…”
Section: The Introduction Of the Gyroscope Monitoring Systemmentioning
confidence: 99%