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Library of Congress Cataloging-in-Publication Data is applied for
ISBN 9781119441885
Cover Design: Wiley
Cover Image: Courtesy of Doruk Senkal
List of Abbreviations
Table 1 Control system abbreviations.
| Symbol | Description |
| Quadrature | Unwanted component of oscillation that interferes with estimation of the pattern angle, manifests as a result of structural imperfections |
| AGC | Amplitude Gain Control, closed‐loop control of drive amplitude |
| PLL | Phase Locked Loop, closed‐loop control system that generates an AC signal with a predetermined phase offset from the resonator |
| FTR | Force‐to‐rebalance, closed‐loop control system that actively drives the pattern angle to a setpoint |
| Quadrature null | Closed‐loop control system that actively suppresses the effects of structural imperfections within the gyroscope |
Table 2 Mechanical parameters of the resonator.
| Symbol | Description |
| f | Mean frequency of the two primary modes of the resonator |
| τ | Mean energy decay time constant of the resonator |
| Q‐factor | Ratio of stored energy to energy loss per vibration cycle (Q = τπf) |
| Δf | Frequency split between primary modes in Hz (Δf = fx − fy) |
| Δω | Frequency split between primary modes in rad/s (Δω = ωx − ωy) |
| Δτ−1 |
Measure of anisodamping within the gyroscope ( |
| θ ω | Angle defining the orientation of actual versus intended axes of elasticity |
| θ τ | Angle defining the orientation of actual versus intended axes of damping |
| (x, y, z) | Coordinate frame oriented along intended axes of symmetry x and y |
| n = 2 mode | A 4‐node degenerate mode pair of a wineglass or ring/disk system |
| n = 3 mode | A 6‐node degenerate mode pair of a wineglass or ring/disk system |
| Precession pattern | Vibration pattern formed by superposition of x and y vibratory modes, which is capable of changing its orientation (precesses) when subjected to Coriolis forces or an external forcing function |
| Pattern angle (θ) | Orientation of the precession pattern in degrees, which is a measure of angular rotation in a Rate Integrating Gyroscope |
Preface
Coriolis Vibratory Gyroscopes (CVGs) can be divided into two broad categories based on the gyroscope's mechanical element: degenerate mode gyroscopes (type 1), which have x–y symmetry, and nondegenerate mode gyroscopes (type 2), which are designed intentionally to be asymmetric in x and y modes.
Currently, nondegenerate mode gyroscopes fulfill the needs of a variety of commercial applications, such as tilt detection, activity tracking, and gaming. However, when it comes to inertial navigation, where sensitivity and stability of the sensors are very important, commercially available MEMS sensors fall short by three orders of magnitude. Degenerate mode gyroscopes, on the other hand, offer a number of unique advantages compared to nondegenerate vibratory rate gyroscopes, including higher rate sensitivity, ability to implement whole‐angle mechanization with mechanically unlimited dynamic range, exceptional scale factor stability, and a potential for self‐calibration. For this reason, as the MEMS gyroscope development is reaching maturity, the Research and Development focus is shifting from high‐volume production of low‐cost nondegenerate mode gyroscopes to high performance degenerate mode gyroscopes. This paradigm shift in MEMS gyroscope research and development creates a need for a reference book to serve both as a guide and an entry point to the field of degenerate mode gyroscopes.
Despite the growing interest in this field, the available information is scattered across a disparate group of conference proceedings and journal papers. For the aspiring scientist/engineer, the scarcity of information forms a large barrier to entry into the field of degenerate mode gyroscopes. This book aims to lower the barrier to entry by providing the reader with a solid understanding of the fundamentals of degenerate mode gyroscopes and its control strategies, as well as providing the necessary know‐how and technical jargon needed to interpret future publications in the field.
The book is intended to be a reference material for researchers, scientists, engineers, and college/graduate students who are interested in inertial sensors. The book may also be of interest to control systems engineers, electrical and electronics engineers, as well as semiconductor engineers who work with inertial sensors. Finally, materials scientists and MEMS production engineers may find the section regarding various fabrication technologies and fabrication defects/energy loss mechanisms interesting.
Doruk Senkal