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基于最大熵准则的多传感器组合导航融合算法OA

Multi-Sensor Integrated Navigation Fusion Algorithm Based on Maximum Correntropy Criterion

中文摘要英文摘要

针对传统的多传感器组合导航系统信息融合方法在非高斯测量噪声下滤波精度下降的问题,本文将基于最大熵准则的卡尔曼滤波器(MCCKF)从单一组合导航系统延伸到多传感器组合导航系统,进而提出了基于最大熵准则(MCC)的序贯式集中融合算法和联邦滤波算法.同时,提出了自适应核带宽的选择方法,以最优化地处理非高斯测量噪声及高斯测量噪声.通过搭建的捷联惯性导航/全球卫星导航/天文导航/大气数据系统(SINS/GNSS/CNS/ADS)组合导航系统进行了算法验证.实验结果表明,基于MCC的序贯式集中融合算法略优于基于MCC的联邦滤波算法.相对于具有容错功能的联邦滤波算法(FT-FKF)及传统集中卡尔曼滤波算法(TCKF),基于MCC的序贯式集中融合算法(MCC-CKF)分别提高位置精度28.4%和20.1%、提高速度精度15.1%和12.7%.

Aiming at the decreasing problem that the filtering accuracy of traditional multi-sensor integrated navigation system information fusion method under non-Gaussian measurement noise,this paper extends Kalman filter based on maximum correntropy criterion(MCCKF)from single integrated navigation system to multi-sensor integrated navigation system,then proposes a sequential centralized fusion algorithm and federated filtering algorithm based on maximum correntropy criterion(MCC).At the same time,it proposes an adaptive kernel bandwidth selection method to optimally deal with non-Gaussian measurement noise and Gaussian measurement noise.The algorithm is verified by the built SINS/GNSS/CNS/ADS integrated navigation system.The experimental results show that the sequential centralized fusion algorithm based on MCC is superior to the federated filtering algorithm based on MCC.Compared with the federated filtering algorithm with fault tolerance function and the traditional centra-lized Kalman filtering algorithm,the sequential centralized fusion algorithm based on MCC can improve position accuracy by 28.4%and 20.1%,and speed accuracy by 15.1%and 12.7%,respectively.

林雪原;潘新龙;李欣

山东外事职业大学,山东 威海 264500海军航空大学,山东 烟台 264000山东外事职业大学,山东 威海 264500

军事科技

最大熵准则卡尔曼滤波器自适应核宽度序贯式集中融合联邦滤波组合导航

maximum correntropy criterionKalman filteradaptive kernel widthsequential centralized fusionfederated filteringintegrated navigation

《航空兵器》 2026 (2)

81-88,8

国家自然科学基金项目(62076249)山东省自然科学基金项目(ZR2020MF154)

10.12132/ISSN.1673-5048.2025.0119

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