Ring laser gyroscope

• US 4,190,364 A
• Filed: 09/07/1977
• Issued: 02/26/1980
• Est. Priority Date: 09/07/1977
• Status: Expired due to Term

• Current Assignee: Kearfott Guidance and Navigation Corporation
• Original Assignee: Singer PLC (Hayleys Plc)
• Inventors: Ljung, Bo H. G., Gamertsfelder, George R.
• Primary Examiner(s): McGraw, Vincent P.
• Application Number:
  US05/831,114
• Time in Patent Office: 902 Days
• Field of Search: 356/106 LR, 356/350
• US Class Current: 356/468
• CPC Class Codes: G01C 19/64 Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
• CPC Class Codes: G01C 19/70 by mechanical means
• CPC Class Codes: H01S 3/0835 Gas ring lasers

Abstract

The invention is concerned with angular rate sensors, and particularly with ring laser gyroscopes which includes means for compensating for the effects of temperature gradients and residual lock-in. A ring laser gyroscope is provided which has a triangular block configuration, and which incorporates a triangular-shaped laser resonant cavity defined by three corner mirrors, including an output mirror. The ring laser gyroscope of the invention includes an optical wedge and a prism attached to its output mirror which permit the center of support of the gyroscope to be located in the plane of symmetry of the block. The gyroscope is mechanically vibrated about its center of gravity to prevent lock-in effects at low angular input rates. The construction of the gyroscope reduces temperature gradients across the plane of symmetry of the instrument, which temperature gradients produce spurious output signals in the absence of an input angular rate. The optical wedge and prism, together with an external corner cube retro-reflector, form an interferometer which provides compensation for the output signal of the gyroscope, enabling the gyroscope to produce an output free from the influence of the mechanical vibrations over a substantial angle, and which permits large angle low frequency mechanical vibrations to be introduced to prevent lock-in effects, which large angle low frequency vibrations have no tendency to cause residual lock-in effects to occur which produce non-linearities in the scale factor of the laser.

Claims

1. A ring laser gyroscope including:

a symmetrical block having a ring laser resonant cavity therein in which two laser beams are created;

reflective means, including an output mirror, mounted on said block for propagating the two laser beams in a closed loop in clockwise and counterclockwise directions around an input axis of the gyroscope;

a support means for the block positioned on the line of symmetry of the block having an axis extending along the input axis of the gyroscope;

resilient means mechanically coupling the block to the support means to permit angular movement of the block around the input axis;

a photodetector;

comepnsating interferometer means for causing the output from the gyroscope to be free from the influence of mechanical vibrations introduced to the block about the input axis over a substantial angular displacement of the block, comprising a stationary retro-reflector, an optical wedge attached to the outer surface of the output mirror, and a prism attached to the outer surface of said wedge for directing one of the laser beams to the retro-reflector and for directing the other laser beam and a reflected beam from the retro-reflector to the photodetector, the laser beam directed to the retro-reflector and the reflected laser beam from the retro-reflector travelling along two parallel paths displaced from one another.

2. The ring laser gyroscope defined in claim 1, and which includes a half-silvered coating on a portion of the surface of said wedge adjacent to said output mirror for directing the reflected beam from the retro-reflector, as reflected by said prism to said half-silvered coating, back into the prism for reflection by the prism to the detector, and for passing the other laser beam into the prism for reflection by the prism to the detector.

3. The ring laser gyroscope defined in claim 1, in which said prism and said optical wedge are attached to one another and to the outer surface of the output mirror by an optical adhesive and said wedge being selected to afford a thermal expansion match so as to avoid optical birefringence due to thermally induced stresses.

4. The ring laser gyroscope defined in claim 1, and which includes an adhesive layer attaching the optical wedge to the output mirror, said adhesive layer having a wedge-shape to form a selected wedge angle between the optical wedge and the output mirror so as to cause the beams incident on said detector to form a predetermined interference pattern.

5. The ring laser gyroscope defined in claim 1, in which said prism is a right-angle prism positioned such that the optical center of said retro-reflector is located on a radius r from the input axis of the gyroscope;

where r=2B/L, and where L is the length of said closed loop, and B is the area enclosed by said enclosed loop.