Dual-axis resonator gyroscope

• US 8,087,295 B2
• Filed: 03/13/2007
• Issued: 01/03/2012
• Est. Priority Date: 03/13/2006
• Status: Active Grant

• Current Assignee: Y-Sensors, Ltd.
• Original Assignee: Yishay Sensors Ltd.
• Inventors: Netzer, Yishay
• Primary Examiner(s): Kwok, Helen C.
• Application Number:
  US12/282,006
• Publication Number:
  US 20090056443A1
• Time in Patent Office: 1,757 Days
• Field of Search: 735/041.2, 735/041.3, 735/041.4, 735/041.5, 735/041.6, 735/040.2, 735/040.4
• US Class Current: 73/504.12
• CPC Class Codes: G01C 19/5719 using planar vibrating masses driven in a translation vibration along an axis

Abstract

The present invention discloses an improved planar, dual-axis, resonator gyroscope with mechanical coupling of adjacent vibrating members. The primary-mode flexible hinges include a tangential torsion element that largely decouples the out-of-plane resonant frequency from the wafer thickness. The use of separate plates for the force-balance and for the electric spring enables decoupling of the two functions. The invention also provides resonant frequency servo-loop for locking of the sense-mode resonant frequency to the drive-mode frequency, an online self-test, a split force balance loop for self cancellation of the quadrature signal, decoupling of the force-balance and resonant frequency servo-loops and stabilization of the inertial rate-sensing sensitivity—when operated in an open loop mode, all without interfering with the normal operation of the gyroscope. An optional sensing of the Z-axis acceleration perpendicular to the sensor plane is also provided which can be used for compensating acceleration-induced errors.

Claims

1. A dual-axis resonator gyroscope comprising:

(a) a baseplate carrying a first set of electrodes; and

(b) a resonator layer deployed above said baseplate, said resonator layer including an anchored portion rigidly attached to said baseplate and four oscillators each linked to said anchored portion via an integral spring formation configured to allow in-plane angular deflection of the corresponding oscillator around an effective center of rotation, said resonator layer further including mechanical linking elements linking between adjacent said oscillators such that, when one of said oscillators undergoes a first angular in-plane deflection, said mechanical linking elements induce an opposite angular in-plane deflection of adjacent ones of said oscillators,

wherein said in-plane angular deflections are excited by means of electrostatic comb drives.

2. The resonator gyroscope of claim 1, wherein each of said oscillators is substantially triangular.

3. The resonator gyroscope of claim 1, wherein a total area of said oscillators corresponds to at least 90 percent of an area of a square encompassing said oscillators.

4. The resonator gyroscope of claim 1, further comprising a coverplate attached to said resonator layer and carrying a second set of electrodes, said first and second sets of electrodes being substantially symmetrical under reflection in plane subdividing a thickness of said resonator layer.