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Ring-laser gyroscope system using dispersive element(s)A ring-laser gyroscope system includes a ring-laser gyroscope (RLG) and at least one dispersive element optically coupled to the RLG's ring-shaped optical path. Each dispersive element has a resonant frequency that is approximately equal to the RLG's lasing frequency. A group index of refraction defined collectively by the dispersive element(s) has (i) a real portion that is greater than zero and less than one, and (ii) an imaginary portion that is less than zero.
Document ID
20100042317
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Smith, David D.
Date Acquired
August 25, 2013
Publication Date
September 28, 2010
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
Patent Number: US-Patent-7,804,600
Patent Application Number: US-Patent-Appl-SN-12/044,740
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,804,600
Patent Application
US-Patent-Appl-SN-12/044,740
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