Design and study of error compensation method for improving the precision of angular rates of nongyro inertial measurement units

被引:2
|
作者
Ding, Mingli [1 ]
Liang, Tingwei [2 ]
Yu, Jintao [3 ]
Wang, Qi [1 ]
机构
[1] Harbin Inst Technol, Dept Automat Testing & Control, Harbin 150001, Peoples R China
[2] Harbin Inst Technol, Dept Aerocraft Dynam & Control, Harbin 150001, Peoples R China
[3] Harbin Univ Commerce, Sch Comp & Informat Engn, Harbin 150028, Peoples R China
来源
基金
中国国家自然科学基金;
关键词
inertial navigation; nongyro; microelectromechanical system accelerometer; angular rate; error compensation; INNOVATIVE ESTIMATION METHOD;
D O I
10.1117/1.3481145
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Nongyro inertial measurement units (NGIMUs) use only microelectromechanical system or microaccelerometers replacing gyroscopes to compute the motion of a moving body. The angular information of NGIMU can be acquired from linear acceleration information. In this work, a new nine-accelerometer configuration of NGIMU is presented with a built experiment system. To improve the precision of the estimated angular rate, a compensation algorithm is used to get the correct accelerometer output. It is provided under the existence of the accelerometer mounting error, which seriously affects NGIMU performance. The simulation study of the proposed methods for estimating the angular rate is investigated based on the present NGIMU configuration. Additionally, the experiment verification using the two-axis turntable to measure the angular rate is also performed. The simulation and experiment results show the feasibility of the configuration and methods. In the experiment, the relative error of this nine-accelerometer configuration is around 1% when the measured angular rate ranges from 0 to 200 deg/s. (c) 2010 Society of Photo-Optical Instrumentation Engineers. [DOI: 10.1117/1.3481145]
引用
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页数:10
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