全球导航卫星系统应用
惯性导航系统
卫星系统
计算机科学
全球导航卫星系统增强
克里金
卡尔曼滤波器
全球定位系统
空中航行
实时计算
人工智能
惯性参考系
电信
机器学习
物理
量子力学
作者
Linzhouting Chen,Zhanchao Liu,Jiancheng Fang
出处
期刊:Journal of Navigation
[Cambridge University Press]
日期:2022-05-23
卷期号:75 (5): 1206-1225
被引量:5
标识
DOI:10.1017/s037346332200025x
摘要
Abstract The integration of the inertial navigation system (INS) and global navigation satellite system (GNSS) is suited for localisation and navigation applications, such as aircrafts, land vehicles and ships. The primary challenge is for navigation system to achieve accurate and reliable navigation solution during GNSS outages. This paper presents an observation prediction methodology for INS/GNSS bridging GNSS outages, which combines partial least squares regression (PLSR) and Gaussian process regression (GPR) to model the INS/GNSS observations and enable a Kalman filter to estimate INS errors. The performance of proposed PLSR/GPR prediction methodology was validated through four GNSS outages taken on flight experiment data, including diverse manoeuvre conditions. The experiment results demonstrate that remarkable performance enhancements are achieved through applying the proposed PLSR/GPR prediction methodology into INS/GNSS integration.
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