Li Jing, Song Ningfang, Yang Gongliu, Jiang Rui
School of Instrumentation Science and Opto-electronics Engineering, Beihang University, 37 Xueyuan Road, Beijing 100191, China.
Rev Sci Instrum. 2016 Jul;87(7):075118. doi: 10.1063/1.4959561.
In the initial alignment process of strapdown inertial navigation system (SINS), large misalignment angles always bring nonlinear problem, which can usually be processed using the scaled unscented Kalman filter (SUKF). In this paper, the problem of large misalignment angles in SINS alignment is further investigated, and the strong tracking scaled unscented Kalman filter (STSUKF) is proposed with fixed parameters to improve convergence speed, while these parameters are artificially constructed and uncertain in real application. To further improve the alignment stability and reduce the parameters selection, this paper proposes a fuzzy adaptive strategy combined with STSUKF (FUZZY-STSUKF). As a result, initial alignment scheme of large misalignment angles based on FUZZY-STSUKF is designed and verified by simulations and turntable experiment. The results show that the scheme improves the accuracy and convergence speed of SINS initial alignment compared with those based on SUKF and STSUKF.
在捷联惯性导航系统(SINS)的初始对准过程中,大失准角总会带来非线性问题,通常可采用尺度无迹卡尔曼滤波器(SUKF)进行处理。本文进一步研究了SINS对准中的大失准角问题,提出了具有固定参数的强跟踪尺度无迹卡尔曼滤波器(STSUKF)以提高收敛速度,然而这些参数是人为构造的且在实际应用中具有不确定性。为进一步提高对准稳定性并减少参数选择,本文提出了一种结合STSUKF的模糊自适应策略(FUZZY - STSUKF)。在此基础上,设计了基于FUZZY - STSUKF的大失准角初始对准方案,并通过仿真和转台实验进行了验证。结果表明,与基于SUKF和STSUKF的方案相比,该方案提高了SINS初始对准的精度和收敛速度。