Low Cost Laser Gyro.
Final rept. on Phase 1,
HONEYWELL INC MINNEAPOLIS MINN SYSTEMS AND RESEARCH CENTER
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The contract was a design study to determine an optimum ring laser gyro size to be used for Army missile applications. As a result of the study, the details of which are presented in this document, a 20 cm path length laser gyro is recommended. The gyro will be operated with the infra-red transition. The lock-in compensation technique will be an alternating bias obtained by use of the transverse Kerr magneto-optic effect at one of the magnetic mirrors.
- Lasers and Masers