Zhao Tianshang, Wang Chenguang, Shen Chong
The State Key Laboratory of Dynamic Measurement Technology, and The School of Instrument and Electronics, North University of China, Taiyuan 030051, China.
Micromachines (Basel). 2023 Oct 15;14(10):1935. doi: 10.3390/mi14101935.
To suppress inertial navigation system drift and improve the seamless navigation capability of microelectromechanical system-inertial navigation systems/geomagnetic navigation systems (MEMS-INS/MNS) in geomagnetically unlocked environments, this paper proposes a hybrid seamless MEMS-INS/MNS strategy combining a strongly tracked square-root cubature Kalman filter with deep self-learning (DSL-STSRCKF). The proposed DSL-STSRCKF method consists of two innovative steps: (i) The relationship between the deep Kalman filter gain and the optimal estimation is established. In this paper, combining the two auxiliary methods of strong tracking filtering and square-root filtering based on singular value decomposition, the heading accuracy error of ST-SRCKF can reach 1.29°, which improves the heading accuracy by 90.10% and 9.20% compared to the traditional single INS and the traditional integrated navigation algorithm and greatly improves the robustness and computational efficiency. (ii) Providing deep self-learning capability for the ST-SRCKF by introducing a nonlinear autoregressive neural network (NARX) with exogenous inputs, which means that the heading accuracy can still reach 1.33° even during the MNS lockout period, and the heading accuracy can be improved by 89.80% compared with the single INS, realizing the continuous high-precision navigation estimation.
为抑制惯性导航系统漂移,提高微机电系统惯性导航系统/地磁导航系统(MEMS-INS/MNS)在地磁解锁环境下的无缝导航能力,本文提出一种将强跟踪平方根容积卡尔曼滤波器与深度自学习相结合的混合无缝MEMS-INS/MNS策略(DSL-STSRCKF)。所提出的DSL-STSRCKF方法包括两个创新步骤:(i)建立深度卡尔曼滤波器增益与最优估计之间的关系。本文结合基于奇异值分解的强跟踪滤波和平方根滤波这两种辅助方法,ST-SRCKF的航向精度误差可达1.29°,与传统单惯性导航系统和传统组合导航算法相比,航向精度分别提高了90.10%和9.20%,大大提高了鲁棒性和计算效率。(ii)通过引入带外部输入的非线性自回归神经网络(NARX)为ST-SRCKF提供深度自学习能力,这意味着即使在地磁导航系统锁定期间,航向精度仍可达到1.33°,与单惯性导航系统相比,航向精度提高了89.80%,实现了连续高精度导航估计。