2019
DOI: 10.1108/sr-05-2018-0133
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A novel multiple-axis MEMS gyroscope-accelerometer with decoupling frames

Abstract: Purpose Technological capabilities of manufacturing microelectromechanical system (MEMS) gyroscopes are still insufficient if compared to manufacturing high-efficient gyroscopes and accelerometers. This creates weaknesses in their mechanical structure and restrictions in the measurement accuracy, stability and reliability of MEMS gyroscopes and accelerometers. This paper aims to develop a new architectural solutions for optimization of MEMS gyroscopes and accelerometers and propose a multi-axis MEMS inertial m… Show more

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Cited by 9 publications
(3 citation statements)
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“…Microstructures based on silicon substrates are, therefore, a key issue in bulk micromachining technology. Bulk Si three-dimensional (3D) micromachined structures (e.g., cavities, grooves, through holes, and mesas) have been an area of extensive research in microelectromechanical systems (MEMS) [1][2][3][4]. From the fabrication point of view, etching techniques are divided into two main categories: deep reactive ion etching (DRIE) and anisotropy wet etching.…”
Section: Introductionmentioning
confidence: 99%
“…Microstructures based on silicon substrates are, therefore, a key issue in bulk micromachining technology. Bulk Si three-dimensional (3D) micromachined structures (e.g., cavities, grooves, through holes, and mesas) have been an area of extensive research in microelectromechanical systems (MEMS) [1][2][3][4]. From the fabrication point of view, etching techniques are divided into two main categories: deep reactive ion etching (DRIE) and anisotropy wet etching.…”
Section: Introductionmentioning
confidence: 99%
“…The bonding temperature is 320°C. The whole flow process is described in more detail in Baranov et al (2019). The manufactured test ESs are shown in Figure 24.…”
Section: Resultsmentioning
confidence: 99%
“…In addition, fields such as navigation [ 2 ], consumer electronics [ 3 ], flight vehicles [ 4 ], and biomechanics [ 5 ] also require the simultaneous measurement of the six spatial components of the acceleration. At present, most of the fields mentioned above use inertial measurement units (IMUs) to measure the space six-axis accelerations of an object, that is, a combined measurement scheme of three linear accelerations and three gyroscopes [ 6 , 7 ]. In general, low-cost IMUs are often limited by gyroscope defects, such as large size, high cost, and large bias instability.…”
Section: Introductionmentioning
confidence: 99%