惯性导航系统
航位推算
卡尔曼滤波器
李群
职位(财务)
数学
控制理论(社会学)
不变(物理)
计算机科学
算法
人工智能
几何学
电信
控制(管理)
经济
全球定位系统
数学物理
方向(向量空间)
财务
作者
Lubin Chang,Hongqiong Tang,Gaoge Hu,Jiangning Xu
出处
期刊:IEEE Transactions on Aerospace and Electronic Systems
[Institute of Electrical and Electronics Engineers]
日期:2023-01-01
卷期号:: 1-17
被引量:2
标识
DOI:10.1109/taes.2023.3285716
摘要
This paper investigates the strapdown inertial navigation system (SINS) initial alignment aided by Doppler velocity log (DVL). A linear Kalman filtering method is proposed using the theory of Lie group, which is immune to the initial misalignment. The dead-reckoning position based on the body velocity provided by DVL and attitude provided by SINS is used as measurement. The SINS calculated attitude, velocity, position and DVL dead-reckoning position are formulated together as the elements of Lie group SE 3 (3). Since the dead-reckoning position is a type of left-invariant measurement, the corresponding linear error-state model is derived based on the left-invariant group error definition. Although the Lie group state model is not group affine, thesmall attitude error assumption does not introduce accuracy degeneracy in deriving the linear error-state model. This is the core reason why the derived linear error-state model is still applicable for cases with large initial misalignment. Experiments are conducted to verify the feasibility and effectiveness of the proposed methods. The test results show that the proposed method has higher accuracy and faster convergence speed as compared with the existing methods.
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