DocumentCode
122363
Title
MRIG frequency mismatch and quadrature control
Author
Lynch, David D.
fYear
2014
fDate
25-26 Feb. 2014
Firstpage
1
Lastpage
4
Abstract
The output variables of an MRIG (Microscale Rate Integrating Gyroscope), x, y, satisfy the equations of motion of a two-dimensional oscillator. (Ref. [1]) To examine the role of a mismatch of the two principal frequencies, ω1 and ω 2, we look at the response to a constant rate input, Ω, for times short compared to the damping time constants. Eqs. (7) of Ref. [1], when specialized to principal-axis coordinates, reduce to x - 2kΩy + ω22 x = 0 (1) ÿ + 2kΩx + ω21 y = 0 when the damping and external-force terms are omitted. k is the angular gain factor. The solution for x(t), y(t) in terms of the initial values x(0), y(0), x(0), y(0) is readily obtained using Laplace transforms. To reduce the writing, we introduce the definitions (Eq. (8) of Ref. [1]).
Keywords
Laplace transforms; damping; gyroscopes; mechanical variables control; motion control; oscillations; Laplace transforms; MRIG frequency mismatch; angular gain factor; constant rate input; damping time constants; external-force terms; microscale rate integrating gyroscope; principal-axis coordinates; quadrature control; two-dimensional oscillator motion; Couplings; Damping; Equations; Force; Frequency control; Mathematical model; Time-frequency analysis;
fLanguage
English
Publisher
ieee
Conference_Titel
Inertial Sensors and Systems (ISISS), 2014 International Symposium on
Conference_Location
Laguna Beach, CA
Type
conf
DOI
10.1109/ISISS.2014.6782503
Filename
6782503
Link To Document