Multiple vibratory rotation sensors with multiplexed electronics

• US 5,892,152 A
• Filed: 07/29/1997
• Issued: 04/06/1999
• Est. Priority Date: 07/29/1997
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Litton Systems Incorporated
• Inventors: Varty, Guy Thomas, Darling, Jeffrey Scott, Schwarz, Robert
• Primary Examiner(s): Williams, Hezron
• Assistant Examiner(s): Kwok, Helen C.
• Application Number:
  US08/901,915
• Time in Patent Office: 616 Days
• Field of Search: 73/504.02, 73/504.03, 73/504.04, 73/504.08, 73/504.13, 73/510, 73/1.77, 73/1.84, 74/5.34, 74/5.4, 74/5.41
• US Class Current: 73/504.13
• CPC Class Codes: G01C 19/5691 of essentially three-dimensional vibrators, e.g. wine glass-type vibrators

Abstract

A vibratory rotation sensor comprising a resonator, a resonator housing and a method for controlling and reading out signals from the sensor is packaged in groups of three, along with a single control and read-out electronics circuit which is either time division multiplexed, frequency multiplexed or a combination of both for the three sensors. This multiple sensor package is compact, lightweight, rugged and well suited for use as an inertial measurement instrument in several subterranean environments such as in mining, tunneling, and oil and gas drilling applications.

Claims

1. An inertial measurement instrument contained within a compact housing, said instrument comprising:

a plurality of vibratory rotation sensors, each sensor having a thin-walled axi-symmetric hemispherical shell resonator capable of vibrating in at least one of a plurality of standing waves;

means associated with each sensor for controlling the amplitude of the standing wave on the resonator in that sensor;

means associated with each sensor for applying excitations to the resonator in that sensor;

means associated with each sensor for reading out information about the standing wave on the resonator in that sensor; and

a multiplexer circuit, connected to said controlling means and said excitation means for selectively activating both said control and excitation means.

2. The inertial measurement instrument of claim 1 wherein said information reading out means comprises an A.C. buffer amplifier connected to the resonators in said plurality of vibratory rotation sensors.

3. The inertial measurement instrument of claim 1 wherein said multiplexer circuit comprises analog switches that connect said control means and said excitation means to only one vibratory rotation sensor at a time.

4. The inertial measurement instrument of claim 3 wherein said control means comprises drive amplifiers and said excitation means comprise drive amplifiers.

5. The inertial measurement instrument of claim 3 wherein said control means and said excitation means comprise the same drive amplifiers.

6. The inertial measurement instrument of claim 3 wherein said analog switches operate at a switching frequency that is a multiple of the gyro operating frequency.

7. The intertial measurement system of claim 1 wherein said multiplexer circuit activates both said control and excitation means on a frequency division basis, with a unique frequency assigned to each one of said sensors.

8. The inertial measurement system of claim 1 wherein said multiplex circuit activates both said control and excitation means on a frequency division basis, with a unique frequency assigned to each one of said sensors, and by time division, connecting said control means and excitation means to only one sensor at a time.

9. The inertial measurement system of claim 8 wherein said line division operates at a switching frequency that is a multiple of the gyro operating frequency.