Noise Characteristics of MEMS Gyro’s Null Drift and Temperature Compensation

doi:10.6180/jase.2012.15.3.04

淡江大學機構典藏 > 工學院 > 航空太空工程學系暨研究所 > 期刊論文 > Item 987654321/83717

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題名:	Noise Characteristics of MEMS Gyro’s Null Drift and Temperature Compensation
作者:	Shiau, Jaw-Kuen;Huang, Chen-Xuan;Chang, Ming-Yu
貢獻者:	淡江大學航空太空工程學系
關鍵詞:	MEMS Gyroscope;Null Drift;Inertial Measurement Unit;Temperature Compensation
日期:	2012-09
上傳時間:	2013-03-20 16:56:26 (UTC+8)
出版者:	Taipei: Tamkang University
摘要:	Gyroscope is one of the primary sensors for air vehicle navigation and controls. This paper investigates the noise characteristics of microelectromechanical systems (MEMS) gyroscope null drift and temperature compensation. This study mainly focuses on temperature as a long-term error source. An in-house-designed inertial measurement unit (IMU) is used to perform temperature effect testing in the study. The IMU is placed into a temperature control chamber. The chamber temperature is controlled to increase from 25 C to 80 C at approximately 0.8 degrees per minute. After that, the temperature is decreased to -40 C and then returns to 25 C. The null voltage measurements clearly demonstrate the rapidly changing short-term random drift and slowly changing long-term drift due to temperature variations. The characteristics of the short-term random drifts are analyzed and represented in probability density functions. A temperature calibration mechanism is established by using an artificial neural network to compensate the long-term drift.With the temperature calibration, the attitude computation problem due to gyro drifts can be improved significantly.
關聯:	Journal of Applied Science and Engineering 15(3), pp.239-246
DOI:	10.6180/jase.2012.15.3.04
顯示於類別:	[航空太空工程學系暨研究所] 期刊論文

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