Title of article
Periodic Error Compensation for Quartz MEMS Gyroscope Drift of INS
Author/Authors
Jianmao، نويسنده , , Xu and Haipeng، نويسنده , , Zhang and Junzhong، نويسنده , , Sun، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2007
Pages
7
From page
539
To page
545
Abstract
In order to improve the navigation accuracy of an inertial navigation system (INS), composed of quartz gyroscopes, the existing real-time compensation methods for periodic errors in quartz gyroscope drift and the periodic error term relationship between sampled original data and smoothed data are reviewed. On the base of the results, a new compensation method called using former period characteristics to compensate latter smoothness data (UFCL for short) method is proposed considering the INS working characteristics. This new method uses the original data without smoothing to work out an error conversion formula at the INS initial alignment time and then compensate the smoothed data errors by way of the formula at the navigation time. Both theoretical analysis and experimental results demonstrate that this method is able to cut down on computational time and raise the accuracy which makes it a better real-time compensation approach for periodic error terms of quartz micro electronic mechanical system (MEMS) gyroscopeʹs zero drift.
Keywords
Real-time compensation , quartz MEMS gyroscope , Periodic error , period characteristic , inertial navigation system (INS)
Journal title
Chinese Journal of Aeronautics
Serial Year
2007
Journal title
Chinese Journal of Aeronautics
Record number
2264685
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