Partially Interacting Multiple-Model Algorithm With Maneuvering Parameters Initialized by Gaussian Mixture

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2025-02-13 DOI:10.1109/TAES.2025.3537071
Gongjian Zhou;Bin Zhu
{"title":"Partially Interacting Multiple-Model Algorithm With Maneuvering Parameters Initialized by Gaussian Mixture","authors":"Gongjian Zhou;Bin Zhu","doi":"10.1109/TAES.2025.3537071","DOIUrl":null,"url":null,"abstract":"The challenge of maneuvering target tracking lies in the difficulty of handling the uncertainty of target motion types and the uncertainty of maneuvering parameters simultaneously. In this article, a partially interacting multiple-model (MM) algorithm with maneuvering parameters initialized by Gaussian mixture (GM-PIMM) is presented. In the proposed method, a maneuver mode is collectively described by multiple models with the same structure and allowing for slight changes in maneuvering parameters. Each model is initialized by a Gaussian probability density function with a quantized mean. The models with the same structure operate independently of each other after parameter initialization, and the interaction between models of different structures is preserved to cope with possible mode jumps. The strategy of initializing maneuvering parameters using the Gaussian mixture eliminates both the mismatch of maneuvering models and the deviation of maneuvering parameters. The mechanism of partial interaction rather than all models interacting with each other protects the best-initialized filter from interference from other incorrectly initialized models, resulting in satisfactory estimation accuracy during maneuver sojourn segments. Simulation results demonstrate the superiority of the proposed GM-PIMM in terms of estimation accuracy and computational complexity compared to the state-of-the-art MM methods.","PeriodicalId":13157,"journal":{"name":"IEEE Transactions on Aerospace and Electronic Systems","volume":"61 3","pages":"7527-7542"},"PeriodicalIF":5.7000,"publicationDate":"2025-02-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Transactions on Aerospace and Electronic Systems","FirstCategoryId":"94","ListUrlMain":"https://ieeexplore.ieee.org/document/10886961/","RegionNum":2,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

Abstract

The challenge of maneuvering target tracking lies in the difficulty of handling the uncertainty of target motion types and the uncertainty of maneuvering parameters simultaneously. In this article, a partially interacting multiple-model (MM) algorithm with maneuvering parameters initialized by Gaussian mixture (GM-PIMM) is presented. In the proposed method, a maneuver mode is collectively described by multiple models with the same structure and allowing for slight changes in maneuvering parameters. Each model is initialized by a Gaussian probability density function with a quantized mean. The models with the same structure operate independently of each other after parameter initialization, and the interaction between models of different structures is preserved to cope with possible mode jumps. The strategy of initializing maneuvering parameters using the Gaussian mixture eliminates both the mismatch of maneuvering models and the deviation of maneuvering parameters. The mechanism of partial interaction rather than all models interacting with each other protects the best-initialized filter from interference from other incorrectly initialized models, resulting in satisfactory estimation accuracy during maneuver sojourn segments. Simulation results demonstrate the superiority of the proposed GM-PIMM in terms of estimation accuracy and computational complexity compared to the state-of-the-art MM methods.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
高斯混合初始化机动参数的部分交互多模型算法
机动目标跟踪的难点在于难以同时处理目标运动类型的不确定性和机动参数的不确定性。提出了一种机动参数由高斯混合初始化的部分交互多模型(GM-PIMM)算法。在该方法中,机动模式由具有相同结构的多个模型共同描述,并允许机动参数的微小变化。每个模型由一个具有量子化均值的高斯概率密度函数初始化。参数初始化后,具有相同结构的模型相互独立运行,并保留了不同结构模型之间的相互作用,以应对可能出现的模态跳变。采用高斯混合初始化机动参数的策略既消除了机动模型的不匹配,又消除了机动参数的偏差。该方法采用部分交互而非所有模型相互作用的机制,保护了最佳初始化滤波器不受其他初始化错误模型的干扰,使机动逗留段的估计精度令人满意。仿真结果表明,该方法在估计精度和计算复杂度方面均优于现有的多目标模型方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
期刊最新文献
Improved Open-Box Array Configuration for 2D Direction Finding by Exploiting Array Motion A Flexible Task Planning Method for Air-Ground Cross-Domain Unmanned Swarm Inspired by Wolf Pack Hunting Behavior Dimensionality-Reduced Virtual Transformation for DOA Estimation in Cylindrical Arrays Modeling and Unilateral Adaptive Control of a Flexible Slung Load System for Multirotor UAV With Actuator Constraints and Faults Deep Neural Network-Based High-Precision Identification of Weak Stability Boundary Structures
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1