High accuracy navigation information estimation for inertial system using the multi-model EKF fusing adams explicit formula applied to underwater gliders. (January 2017)

• Record Type: Journal Article
• Authors: Huang, Haoqian; Chen, Xiyuan; Zhang, Bo; Wang, Jian
• Is Part Of: ISA transactions. Volume 66(2017:Jan.)
• Page Start: 414
• Page End: 424
• Publication Date: 2017-01
• Subjects: Underwater glider -- Inertial navigation system -- Error estimation -- Multi-model -- Adams formula; Engineering instruments -- Periodicals; Engineering instruments; Periodicals; Electronic journals; 629.805
• DOI: 10.1016/j.isatra.2016.10.020
• Languages: English
• ISSNs: 0019-0578

Abstract

Abstract: The underwater navigation system, mainly consisting of MEMS inertial sensors, is a key technology for the wide application of underwater gliders and plays an important role in achieving high accuracy navigation and positioning for a long time of period. However, the navigation errors will accumulate over time because of the inherent errors of inertial sensors, especially for MEMS grade IMU (Inertial Measurement Unit) generally used in gliders. The dead reckoning module is added to compensate the errors. In the complicated underwater environment, the performance of MEMS sensors is degraded sharply and the errors will become much larger. It is difficult to establish the accurate and fixed error model for the inertial sensor. Therefore, it is very hard to improve the accuracy of navigation information calculated by sensors. In order to solve the problem mentioned, the more suitable filter which integrates the multi-model method with an EKF approach can be designed according to different error models to give the optimal estimation for the state. The key parameters of error models can be used to determine the corresponding filter. The Adams explicit formula which has an advantage of high precision prediction is simultaneously fused into the above filter to achieve the much more improvement in attitudes estimation accuracy. The proposed algorithm has been proved through theory analyses and has been tested by both vehicle experiments and lake trials. Results show that the proposed method has better accuracy and effectiveness in terms of attitudes estimation compared with other methods mentioned in the paper for inertial navigation applied to underwater gliders. Highlights: A novel multi-model EKF filter is proposed to perform the optimal estimation. A novel fusion method integrating the Adams explicit formula with the multi-model EKF is proposed. The performance of method is verified in the application of underwater glider successfully.