Vibratory angular rate sensor

• US 6,155,115 A
• Filed: 01/14/1993
• Issued: 12/05/2000
• Est. Priority Date: 01/02/1991
• Status: Expired due to Fees

• Current Assignee: Per Ljung
• Original Assignee: Per Ljung
• Inventors: Ljung, Per
• Primary Examiner(s): CHAPMAN JR, JOHN E
• Application Number:
  US08/005,197
• Time in Patent Office: 2,882 Days
• Field of Search: 73/505, 73/504.12
• 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

A single-axis angular rate sensor is comprised of a transducer and associated electronics. The transducer consists of a symmetric planar inertia member supported by symmetrically disposed coplanar elastic beams. The inertia member is angularly oscillated about its center of gravity about a first axis. Rotation of the sensor about a third orthogonal axis results in Coriolis moments, causing angular oscillations about an orthogonal second axis. The angular oscillations about the second axis are restrained by means of voltages applied to electrostatic electrodes. These voltages are proportional to the angular input rate.

Claims

1. An inertial sensor comprising:

an inertia member extending substantially in a plane,

a first and second reference axes extending in said plane and a third reference axis extending perpendicular to the plane, said three reference axes being mutually perpendicular and intersecting the center of gravity of said inertia member,

suspension means connecting the inertia member to a support for supporting the inertia member in said plane,

wherein said suspension means comprises four elastic beams extending substantially in said plane between said support and said inertia member, the longitudinal axes of said beams intersecting said center of gravity,

said elastic beams allowing limited angular motion of said inertia member about said reference axes;

electrostatic driving means to drive said inertia member in an angular oscillatory motion about said first reference axis; and

electrostatic sensing means for sensing angular oscillatory motion of the inertia member about the second reference axis, said angular oscillatory motion caused by Coriolis forces due to angular rotation of the inertial sensor about said third reference axis.

2. An inertial sensor according to claim 1, further comprising:

means to substantially restrain oscillatory angular motion of said inertia member about said second reference axis, wherein said means to restrain the motion generates a signal representative of the torque required to restrain the motion.

3. An inertial sensor according to claim 2, wherein said driving, sensing and restraining means comprise coplanar electrostatic elements.