Vibration-Induced Drift in the Hemispherical Resonator Gyro

David D. Lynch

Abstract:	The mechanisms in the HRG that lead to drift sensitivity to externally applied vibration arc discussed. They are shown to result in modest vibration sensitivities that occur only at frequencies above those of the usual aircraft vibration environment. The HRG is shown to be suitable for use in severe vibration environments.
Published in:	Proceedings of the 43rd Annual Meeting of The Institute of Navigation (1987) June 23 - 25, 1987 Dayton, Ohio
Pages:	34 - 37
Cite this article:	Lynch, David D., "Vibration-Induced Drift in the Hemispherical Resonator Gyro," Proceedings of the 43rd Annual Meeting of The Institute of Navigation (1987), Dayton, Ohio, June 1987, pp. 34-37.
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