Stimulated rate optical power measurement in a fiber optic gyroscope

• US 7,274,460 B2
• Filed: 06/02/2004
• Issued: 09/25/2007
• Est. Priority Date: 06/02/2004
• Status: Active Grant

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Northrop Grumman Corporation
• Inventors: Bowser, Mark P.
• Primary Examiner(s): Lyons; Michael A.
• Application Number:
  US10/859,822
• Publication Number:
  US 20050270540A1
• Time in Patent Office: 1,210 Days
• Field of Search: 356/460, 356/462, 356/463, 356/464, 250/227.19, 250/227.27, 385/12
• US Class Current: 356/460
• CPC Class Codes: G01C 19/72 with counter-rotating light beams in a passive ring, e.g. fibre laser gyrometers

Abstract

Fiber optic gyroscopes having integrated power measurement capabilities and related methods and apparatus. More particularly, fiber optic gyroscopes having an integrated method for determining the optical power by applying an electronic stimulated rate internal to the closed loop digital electronics of the gyroscopes and monitoring the counts out per second (COPS) using each gyroscope'"'"'s counts output signal. Knowing a COPS value, the optical power can be determined by dividing a constant K by the COPS value, i.e. Optical Power=K/COPS. The value of K is specific to each gyroscope, and can be calculated or measured.

Claims

1. A method of determining performance, or life expectancy of a fiber optic gyroscope comprising:

simulating movement of the gyroscope;

monitoring an output of the gyroscope during said simulation;

using the monitored output to calculate an optical power value for the gyroscope; and

determining life expectancy of the gyroscope using the calculated optical power value.

2. The method of claim 1 wherein the monitored output is a value proportional to an angular velocity of the gyroscope.

3. The method of claim 2 wherein simulating movement of the gyroscope comprises providing a rate value to the gyroscope that causes the gyroscope to output an angular velocity value equivalent to the value it would output if the gyroscope were physically rotating at the provided rate.

4. The method of claim 3 wherein the provided rate value is added to a value corresponding to a phase difference between two counterpropagating light beams.

5. The method of claim 4 wherein using the monitored output to calculate an optical power value comprises dividing a predetermined constant by the value of the monitored output.

6. The method of claim 1 comprising:

determining a counts output per second value for the gyroscope; and

determining the optical power of the gyroscope, at least in part, from the counts output per second value.

7. The method of claim 6 further comprising determining a value K for the gyroscope, and determining the optical power of the gyroscope, at least in part, from both K and the counts output per second value.

8. The method of claim 7 wherein determining the optical power of the gyroscope comprises determining the value of K divided by the counts output per second 9value.

9. The method of claim 8 wherein determining the value of K comprises calculating the value from a plurality of factors that include one or more of the following:

modulation amplitude, optical receiver transimpedance, preamplifier gains, filter gains, A/D converter least significant bit, and the size of the stimulated rate bit.

10. The method of claim 8 wherein determining the value of K comprises obtaining an optical power value and a corresponding counts output per second value and using the ratio of the optical power value to the counts output per second value as K.

11. A closed loop interferometer fiber optic gyroscope comprising:

a synchronous detector;

an integrator; and

means for introducing a simulated rate diagnostic signal in between the synchronous detector and the integrator, creating a DC steady state disturbance in the closed loop, as if an input angular rate had been applied to the fiber optic gyroscope.

12. The gyroscope of claim 11 further comprising:

means to provide an output value equal to the optical power of the gyroscope in response to an external request, by internally specifying the rate and using the resultant counts value to compute the optical power output value.

13. The gyroscope of claim 12 further comprising means for storing a rate and a constant value to be used in response to an external request for the optical power value.