Inertial unit having vibrating gyros mounted on a carousel, and an angle-measurement method

• US 9,279,682 B2
• Filed: 05/23/2013
• Issued: 03/08/2016
• Est. Priority Date: 05/24/2012
• Status: Active Grant

• Current Assignee: Safran Electronics & Defense
• Original Assignee: Sagem Defense Securite SA (Safran SA)
• Inventors: Lignon, Christian, Renault, Alain, Brunstein, Etienne
• Primary Examiner(s): KWOK, HELEN C
• Application Number:
  US13/901,144
• Publication Number:
  US 20130312518A1
• Time in Patent Office: 1,020 Days
• Field of Search: 735/040.8, 734/93, 735/10, 735/11, 735/041.2
• US Class Current: 1/1
• CPC Class Codes: G01C 19/04 Details
• CPC Class Codes: G01C 19/5691 of essentially three-dimensional vibrators, e.g. wine glass-type vibrators
• CPC Class Codes: G01P 1/02 Housings

Abstract

An inertial unit comprising an inertial core (3) that is connected to a control unit (50) and that includes three gyros (9, 10, 11) that are mounted relative to one another so as to have sensing axes (X, Y, Z) that are substantially perpendicular to one another, the gyros being vibrating axisymmetric gyros with hemispherical resonators, the unit being characterized in that the core is mounted on a carousel (2) arranged to drive the inertial core in rotation about an axis of rotation (4) at at least one frequency that corresponds to a minimum for spectral error density of the gyros. An angle-measurement method making use of the unit.

Claims

1. An inertial unit comprising an inertial core that is connected to a control unit and that includes three gyros that are mounted relative to one another so as to have sensing axes that are substantially perpendicular to one another, the gyros being vibrating axisymmetric gyros with hemispherical resonators, wherein the inertial core is mounted on a carousel arranged to drive the inertial core in rotation about an axis of rotation at at least one predetermined frequency of rotation and wherein the axis of rotation coincides with a trisector of the sensing axes.

2. An inertial unit according to claim 1, wherein the carousel is arranged to cause the inertial core to perform continuous rotary motion.

3. An inertial unit according to claim 1, wherein the carousel is arranged to cause the inertial core to perform alternating rotary motion.

4. An inertial unit according to claim 1, wherein the carousel is positioned so that the axis of rotation is vertical.

5. An inertial unit according to claim 1, wherein the carousel is positioned so that the axis of rotation is horizontal.

6. An angle-measurement method making use of the inertial unit in accordance with any one of claims 1 and 2-5, the method comprising the steps of:

causing the carousel to rotate about the axis of rotation; and

taking measurements with each gyro during rotation of the carousel.

7. A method according to claim 6, wherein a measurement operation is performed continuously during rotation.

8. A method according to claim 6, wherein the axis of rotation is such that the gyros have errors that appear at frequencies that are not identical and the frequencies at which the gyro errors appear are not harmonics of one another, and wherein a step is performed of allocating errors to the gyros as a function of the frequencies at which the errors appear.