The present investigation of FOG behavior under vibration conditions gives attention to effective techniques for vibration-compensation. The FOGs tested are noted to yield an intermediate level of performance, of the order of 3 deg/hr at 1-sigma, under commonly encountered vibration conditions and over the temperature range associated with aerospace applications. These FOGs have been deemed adequate for use in the triaxial inertial devices of the guidance and control system aboard the TR-1 rocket.
Development of fiber optic gyroscope with environmental ruggedness
Fiber Optic Gyros: 15th Anniversary Conf ; 1991 ; Boston,MA,United States
Proc. SPIE ; 1585 ; 82
01.02.1992
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Online Contents | 1994
|Interferometric Fiber-Optic Gyroscope
NTRS | 1990
|Progress in passive fiber optic gyroscope development
British Library Conference Proceedings | 1994
|Phase Conjugate Fiber Optic Gyroscope
British Library Online Contents | 2014
|Fiber optic gyroscope north finder
British Library Conference Proceedings | 1994
|