Abstract
This paper considers the dependence of the rotor tuning condition of a rotor-vibratory gyroscope on the elastic properties of the spring element which has, in particular, additional angular deflection along an axis perpendicular to the output axis of gyroscope. As a consequence of this dependence, the limitations to the performance of the rotor tuning condition are examined and a mathematical equation describing the rotor tuning error, dependent on variations in the gyroscope parameters, is obtained. Analysis of the equation of rotor tuning error allows us to formulate the condition needed for minimization of this error against temperature change.
Original language | English |
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Article number | 5699329 |
Pages (from-to) | 1856-1860 |
Number of pages | 5 |
Journal | IEEE Sensors Journal |
Volume | 11 |
Issue number | 9 |
Early online date | 20 Jan 2011 |
DOIs | |
Publication status | Published - 30 Sept 2011 |
Bibliographical note
Funding Information:The authors acknowledge with thanks the support of the Arzamas Research and Production Joint Stock Company “Temp-Avia.”
Keywords
- Angular rate
- gyroscope
- inertial sensor
ASJC Scopus subject areas
- Instrumentation
- Electrical and Electronic Engineering