首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于相对导航的多平台INS误差联合修正方法
引用本文:张共愿,程咏梅,程承,杨峰,雷宝权.基于相对导航的多平台INS误差联合修正方法[J].航空学报,2011,32(2):271-280.
作者姓名:张共愿  程咏梅  程承  杨峰  雷宝权
作者单位:1. 西北工业大学自动化学院,陕西西安,710129
2. 西安飞行自动控制研究所,陕西西安,710065
基金项目:国家自然科学基金,航空科学基金,西北工业大学研究生创业种子基金,西北工业大学翱翔之星计划
摘    要:在机群协同编队飞行中,编队成员仅装载惯性导航系统(INS)的方式具有隐蔽、抗干扰等明显的优势,但随着航时的增加,INS误差将不断累积.使导航系统失效,为此,提出基于相对导航的多平台INS误差联合修正方法.首先,建立了编队成员相对导航运动模型及非线性观测模型,采用量测重构技术构造了伪线性观测模型并推导了观测噪声协方差矩阵...

关 键 词:协同编队  相对导航  惯性导航  伪线性  扩展卡尔曼滤波

A Joint Correcting Method of Multi-platform INS Error Based on Relative Navigation
ZHANG Gongyuan,CHENG Yongmei,CHENG Cheng,YANG Feng,LEI Baoquan.A Joint Correcting Method of Multi-platform INS Error Based on Relative Navigation[J].Acta Aeronautica et Astronautica Sinica,2011,32(2):271-280.
Authors:ZHANG Gongyuan  CHENG Yongmei  CHENG Cheng  YANG Feng  LEI Baoquan
Institution:1.College of Automation,Northwestern Polytechnical University,Xi’an 710129,China 2.Flight Automatic Control Research Institute,Xi’an 710065,China
Abstract:It is of distinct advantage that the members of an air fleet are equipped with just inertial navigation system (INS) in collaborative formation flying, such as concealment, anti-jamming,etc. However, with the increase of endurance, INS error will be cumulated continuously, which may lead the navigation system to fail. Therefore, this article proposes a joint correcting method of multi-platform INS errors based on relative navigation. First, it builds a relative motion model and a nonlinear observation model, constructed a pseudo linear observation model with measurement reconstruct technique, and then it deduces the pseudo linear observation covariance matrix. Second, the article proposes a joint correcting method of multi-platform INS errors based on relative navigation, and demonstrates the satisfactory effect of this joint INS error correction. Furthermore, it provides a specific strategy of joint correction. Finally, the simulation result shows that compared with the extended Kalman filter (EKF), the proposed method can increase the convergence rate of relative navigation by a large amount while the accuracy remains unchanged on the whole. The joint correcting method of multi-platform INS errors based on relative navigation effectively slows down the divergence speed of INS errors of a formation system.
Keywords:collaborative formation  relative navigation  inertial navigation  pseudo linearity  extended Kalman filter
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号