CA1339667C - Appareil et methode pour corriger les erreurs d'angle de phase d'un gyrolaser annulaire dues a l'accrochage
- Google Patents
Appareil et methode pour corriger les erreurs d'angle de phase d'un gyrolaser annulaire dues a l'accrochage
Info
Publication number
CA1339667C
CA1339667CCA 581408CA581408ACA1339667CCA 1339667 CCA1339667 CCA 1339667CCA 581408 CA581408 CA 581408CA 581408 ACA581408 ACA 581408ACA 1339667 CCA1339667 CCA 1339667C
Authority
CA
Canada
Prior art keywords
signal
ring laser
laser gyroscope
phase
lock
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Northrop Grumman Guidance and Electronics Co Inc
Original Assignee
Litton Systems Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US07/110,003external-prioritypatent/US5347359A/en
Application filed by Litton Systems IncfiledCriticalLitton Systems Inc
Application grantedgrantedCritical
Publication of CA1339667CpublicationCriticalpatent/CA1339667C/fr
CA 5814081987-10-191988-10-27Appareil et methode pour corriger les erreurs d'angle de phase d'un gyrolaser annulaire dues a l'accrochage
Expired - Fee RelatedCA1339667C
(fr)
Apparatus and method for detecting rotation rate and direction of rotation and providing cavity length control in multioscillator ring laser gyroscopes