2022
DOI: 10.1016/j.sna.2022.113539
|View full text |Cite
|
Sign up to set email alerts
|

Effects of electrostatic nonlinearity on the rate measuring performance of ring based Coriolis Vibrating Gyroscopes (CVGs)

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

2022
2022
2024
2024

Publication Types

Select...
4
1

Relationship

0
5

Authors

Journals

citations
Cited by 5 publications
(2 citation statements)
references
References 19 publications
0
2
0
Order By: Relevance
“…For example, a frequency split of Δf = 1 Hz results in a bias error of 360°/s [ 57 ]. The deviation of the sensor from its mean value of the output rate is called the bias stability (or bias instability), the zero-bias error [ 59 ], or the signal-to-noise ratio, which is a measure of the gyroscope stability over a specified period of time or quality of measurement [ 62 ]. Bias instability, which is a performance quality measurement of gyroscopes, is a drift of the measurement from the average value, also called the drift angle or bias drift, and has a unit of degree/h.…”
Section: Theory and Performance Of Hrgmentioning
confidence: 99%
“…For example, a frequency split of Δf = 1 Hz results in a bias error of 360°/s [ 57 ]. The deviation of the sensor from its mean value of the output rate is called the bias stability (or bias instability), the zero-bias error [ 59 ], or the signal-to-noise ratio, which is a measure of the gyroscope stability over a specified period of time or quality of measurement [ 62 ]. Bias instability, which is a performance quality measurement of gyroscopes, is a drift of the measurement from the average value, also called the drift angle or bias drift, and has a unit of degree/h.…”
Section: Theory and Performance Of Hrgmentioning
confidence: 99%
“…However, for Type I gyroscopes with identical drive and sense modes, it is essential that their resonant structures possess impeccable symmetry 7 . Unfortunately, due to manufacturing imperfections, the fabricated gyroscope's resonant structure is not perfectly symmetrical due to the non-uniform distribution of crucial structural parameters such as stiffness and damping 8 . Consequently, the primary sources of errors that impact gyroscope performance stem from the asymmetry in stiffness and damping.…”
Section: Introductionmentioning
confidence: 99%