Design of MEMS gyroscope interface ASIC with on-chip temperature compensation
H Zhang, W Chen, L Yin, Q Fu - Measurement, 2023 - Elsevier
Zero bias and scale factor are important overall performance indicators for micromechanical
gyroscopes and are commonly used to describe the temperature stability of MEMS …
gyroscopes and are commonly used to describe the temperature stability of MEMS …
A mode-matched DRG realized by monolithic integrated interface circuit design
Y Wang, X Liu, W Zhang, Y Zhang… - IEEE Sensors Journal, 2022 - ieeexplore.ieee.org
This article proposes a novel design method for the mode-matched disk resonator
gyroscope (DRG) realized by the monolithic integrated interface circuit. The mode …
gyroscope (DRG) realized by the monolithic integrated interface circuit. The mode …
Monolithic Integrated Interface ASIC with Quadrature Error Correction for MEMS Dual-Mass Vibration Gyroscope
H Zhang, L Yin, W Chen, Q Fu… - IEEE Sensors Journal, 2024 - ieeexplore.ieee.org
A novel design method of a monolithic integrated interface circuit with quadrature error
correction for a microelectromechanical system (MEMS) dual-mass vibratory gyroscope is …
correction for a microelectromechanical system (MEMS) dual-mass vibratory gyroscope is …
Study of the influence of phase noise on the MEMS disk resonator gyroscope interface circuit
W Zhang, W Chen, L Yin, X Di, D Chen, Q Fu, Y Zhang… - Sensors, 2020 - mdpi.com
In this paper, a detailed analysis of the influence of phase noise on the micro-electro-
mechanical system (MEMS) disk resonator gyroscope (DRG) is presented. Firstly, a new …
mechanical system (MEMS) disk resonator gyroscope (DRG) is presented. Firstly, a new …
[PDF][PDF] Aircraft Attitude Determination Algorithms Employing Gravity Vector Estimations and Velocity Measurements.
Precision on Navigation, Guidance and Control of aircraft is dependent on the precision of
the measurement system both for position and attitude. It is well known in aerospace …
the measurement system both for position and attitude. It is well known in aerospace …
An ASIC Interface for MEMS Vibratory Gyroscopes With a 110 dB DR and 0.001° s/√ Hz Noise Floor Over a 100 Hz
S Long, S Ma, X Fan, C Wu, Z Tong… - 2023 8th International …, 2023 - ieeexplore.ieee.org
This paper presents an ASIC interface for MEMS vibratory gyroscopes with a wide tuning
range from 5 kHz to 20 kHz. This ASIC interface integrates a sense open-loop module, a …
range from 5 kHz to 20 kHz. This ASIC interface integrates a sense open-loop module, a …
A Simplified Method to Determine Gravity Vector Through Aerodynamic Coefficients and its Applications in Attitude Determination
Position and attitude determine the accuracy on the navigation and control of any airship.
The possibility of determining the rotation of a body is provided by the measurements of two …
The possibility of determining the rotation of a body is provided by the measurements of two …
∑-Δ based force-feedback capacitive micro-machined sensors: Extending the input signal range
Operating MEMS capacitive sensors in negative feedback mode results in improved
bandwidth, and lower sensitivity to process and temperature variation. Feedback operation …
bandwidth, and lower sensitivity to process and temperature variation. Feedback operation …
A self-clocked readout circuit for MEMS gyroscope to avoid frequency aliasing
L Jiang, D **ao, Z Chen, Q Xu, S Guan… - 2016 IEEE …, 2016 - ieeexplore.ieee.org
The performance of MEMS gyroscope is susceptible to the interface circuits. It is reported in
the published literature that traditional interface circuits adopted modulation and …
the published literature that traditional interface circuits adopted modulation and …