PASSIVE RING RESONATOR GYROSCOPE
Assignee
Rockwell International
Filed as: ROCKWELL INTERNATIONAL CORPORATION
Filed
Nov 29, 1984
Granted
Jun 2, 1992
Location
LAGUNA HILLS CA US
Abstract
A passive ring resonator gyroscope comprising a single piece body having an integral first and second resonator cavity. The first resonator cavity has a single frequency laser means with internal cavity mounted reflective surfaces to provide a single frequency light source to the second resonator cavity. The single frequency light source is sharply tuned. The second resonator cavity is a passive high Q evacuated cavity having a closed second optical path tuned to resonate at the single frequency light frequency of the first resonator cavity. A cavity servo means is provided for controlling the resonant frequency of the second resonator high Q cavity to simultaneously and substantially track the resonant frequency of the first resonator high Q cavity. An output servo means is provided for detecting the change in frequency of the single frequency light within the second resonator in response to said body rate input to the sensitive axis and for providing an output signal.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Jan 28, 1987
Rescinded
Aug 16, 1991
Duration
4 years, 6 months
Inventor
- 1VIRGIL E. SANDERS
Technology Domains
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Record Details
- Patent number
- US 5118189
- Application
- 06676322
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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