Optimization of redundant configuration scheme for vehicle inertial sensors with high reliability

被引:0
作者
Yuan Y. [1 ]
Zou B. [1 ]
机构
[1] School of Automotive Engineering, Wuhan University of Technology, Wuhan
来源
Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University | 2018年 / 39卷 / 08期
关键词
Accuracy; Generalized likelihood test; Linear prediction; Micro-vehicle; Multiple faults detection and isolation; Orthogonal cone configuration; Redundancy configuration; Reliability; Strapdown inertial navigation technology;
D O I
10.11990/jheu.201801055
中图分类号
学科分类号
摘要
In the three-axis orthogonal configuration of a strapdown inertial navigation system, a single gyroscope fault can directly lead to system failure. To address this, a redundant configuration scheme with high reliability is proposed for vehicle inertial sensors, based on orthogonal cone redundancy configuration. First, to achieve a higher reliability, better navigation performance, and higher precision under a single fault condition, a five-gyro orthogonal cone configuration was designed. Then, a fault detection and isolation method was designed based on the combination of generalized likelihood test fault detection and linear prediction isolation method, which solved the problems of multi-fault detection and isolation. The performance simulation shows that the new optimal solution of redundant configuration for vehicle inertial sensors improves system reliability 1.35 times more than non-redundant configuration, and can accurately detect and isolate multiple faults in redundant system, which has an important application value in the project design of micro-vehicle inertial strapdown systems. © 2018, Editorial Department of Journal of HEU. All right reserved.
引用
收藏
页码:1369 / 1375
页数:6
相关论文
共 17 条
[1]  
Jafari M., Roshanian J., Inertial navigation accuracy increasing using redundant sensors, Journal of Science and Engineering, 1, 1, pp. 55-66, (2013)
[2]  
Zou B., Tan L., Hou X., Drivable road regions detection based on Lidar, Journal of Wuhan University of Technology (transportation Science & Engineering), 41, 2, pp. 203-207, (2017)
[3]  
Cheng J., Dong J., Landry R., Et al., A novel optimal configuration form redundant MEMS inertial sensors based on the orthogonal rotation method, Sensors, 14, 8, pp. 13661-13678, (2014)
[4]  
Shim D.S., Yang C.K., Optimal configuration of redundant inertial sensors for navigation and FDI performance, Sensors, 10, 7, pp. 6497-6512, (2009)
[5]  
Yang C.K., Shim D.S., Accommodation rule based on navigation accuracy for double faults in redundant inertial sensor systems, International Journal of Control Automation and Systems, 5, 3, pp. 329-336, (2007)
[6]  
Wang J., Zhang M., A strapdown IMU configuration with high reliability, Journal of Chinese Inertial Technology, 20, 3, pp. 363-367, (2012)
[7]  
Liang H., Key technique of micro inertial system based on redundant gyroscopes, (2011)
[8]  
Yang H., Zhang S., Cai H., An in-flight calibration for redundant inertial measurement gyroscope, Journal of Astronautics, 31, 1, pp. 104-110, (2010)
[9]  
Huang J., Fu W., Chen K., Et al., Redundant Configuration and optimization of storapdown inertial measurement unit, Command Control and Simulation, 35, 6, pp. 105-108, (2013)
[10]  
Yan H., Chen J., Liu X., Application of redundancy technology in inertial navigation systems, Journal of Chinese Inertial Technology, 11, 3, pp. 68-72, (2003)