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 …
[HTML][HTML] 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.
R de Celis, L Cadarso - ICINCO (1), 2017 - pdfs.semanticscholar.org
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
R de Celis, L Cadarso - Informatics in Control, Automation and Robotics …, 2020 - Springer
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 Xiao, 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 …