2021
DOI: 10.3390/mi12080902
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Design Approach for Reducing Cross-Axis Sensitivity in a Single-Drive Multi-Axis MEMS Gyroscope

Abstract: In this paper, a new design technique is presented to estimate and reduce the cross-axis sensitivity (CAS) in a single-drive multi-axis microelectromechanical systems (MEMS) gyroscope. A simplified single-drive multi-axis MEMS gyroscope, based on a mode-split approach, was analyzed for cross-axis sensitivity using COMSOL Multiphysics. A design technique named the “ratio-matching method” of drive displacement amplitudes and sense frequency differences ratios was proposed to reduce the cross-axis sensitivity. In… Show more

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Cited by 6 publications
(5 citation statements)
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“…On the other hand, when measurement tools are present (in this case, angular speed sensors and angle sensors), ( 13) is rewritten as (14). Based on the diagnostic analysis results obtained from the system ( 14), we can accurately identify the exact time of failure during parameter measurement or calculation.…”
Section: Determine Aircraft Control System Failures 21 System Overviewmentioning
confidence: 99%
See 1 more Smart Citation
“…On the other hand, when measurement tools are present (in this case, angular speed sensors and angle sensors), ( 13) is rewritten as (14). Based on the diagnostic analysis results obtained from the system ( 14), we can accurately identify the exact time of failure during parameter measurement or calculation.…”
Section: Determine Aircraft Control System Failures 21 System Overviewmentioning
confidence: 99%
“…Then it is necessary to determine the failure parameters and methods to fix the failure of the sensor system. The status of other components of the ACS is determined similarly [14].…”
Section: Introductionmentioning
confidence: 99%
“…In this section, we compare the performance characteristics of previously reported high-precision micro-opto-electro-mechanical systems (MOEMS) gyroscopes to our novel dual-frame optomechanical gyroscope architecture incorporating an integrated photonic crystal cavity. As summarized in Table 3, three earlier frame-type MEMS gyroscope designs utilized an electrostatic comb drive actuator and displacement sensor [39,42,43]. However, these approaches exhibited limitations associated with electronic noise introduced by the driving and sensing methods employing different operating modes.…”
Section: Comparative Studymentioning
confidence: 99%
“…Temperature-induced errors occur due to changes in the material properties of the selected material and electronic parts. In MEMS sensors, temperature-induced errors result in several other errors, such as spring softening, resonant frequency error, cross-axis sensitivity, and bias instability [ 17 , 18 , 19 , 20 ]. Among all the high-performance MEMS gyroscope specifications, bias stability is the first thing system designers must ensure to deliver performance [ 21 ].…”
Section: Introductionmentioning
confidence: 99%