首页期刊简介编委会征稿启事出版道德声明审稿流程读者订阅论文查重联系我们English
引用本文
  • 马 霞,王永胜.SINS/GPS/TACAN机载综合导航定位系统设计[J].电讯技术,2011,51(4): - .    [点击复制]
  • MA Xia,WANG Yong-sheng.Design of an Airborne Integrated Navigation and Location System Based on SINS/GPS/TACAN[J].,2011,51(4): - .   [点击复制]
【打印本页】 【下载PDF全文】 查看/发表评论下载PDF阅读器关闭

←前一篇|后一篇→

过刊浏览    高级检索

本文已被:浏览 2276次   下载 1569 本文二维码信息
码上扫一扫!
SINS/GPS/TACAN机载综合导航定位系统设计
马霞,王永胜
0
(中国西南电子技术研究所,成都 610036;北京市9236信箱,北京 100036)
摘要:
在现代空战中,捷联惯性导航系统(SINS)、全球定位系统(GPS)和塔康(TACAN) ,单独利用各导航信息都存在着弊端。为此,提出了3种导航源综合的导航系统设计方案。 信息融合技术采用广义联邦滤波技术来完成,状态矢量为导航参数误差,并建立准确数学模 型。各个子滤波器(局部滤波器)采用间接滤波方式工作,完成状态矢量局部估算;主滤波 器(全局滤波器)进行子滤波器的公共状态矢量融合和时间更新,输出可靠、准确的导航参 数误差的全局最优估计量。利用全局滤波输出作为闭环负反馈校正SINS导航源,实现动态校 正(比力方程积分初始条件重新设置)、动态对准(姿态矩阵微分方程积分初始条件重新设 置)和动态标定,从而提高了组合导航系统性能。系统试验表明,SINS/GPS/TACAN综合导 航定位系统获得了良好的定位精度。
关键词:  综合导航  联邦滤波  SINS  GPS  TACAN
DOI:
基金项目:
Design of an Airborne Integrated Navigation and Location System Based on SINS/GPS/TACAN
MA Xia,WANG Yong-sheng
(Southwest China Institute of Electronic Technology,Chengdu 610036,China;Beijing P.O. Box 9236,Beijing 100036,China)
Abstract:
In modern air warfare,independent use of strap down inertial system(SINS), glob al po sition system(GPS) and tactical air navigation system(TACAN) has disadvantages. In this paper the airborne integrated navigation system is proposed based on th ese three navigation equipment . The information fusion is accomplished by using federated filtering technolog y, choosing the error of navigation parameter as the state vector, and construct ing the mathematics model of state equation about integrated system. Each of sub filters gains an estimation of state vector by using work method of indirect f ilter.Primary filter accomplishes the fusion of public state vectors about sub filters and time updating, and outputs the credible, precise and optimal estim ation of navigation parameter error. Using the output of the whole filter as mea ns o f closed loop of feeding back, correct inertial navigation parameter, dynamic calibration(reinstalling the integral initial condition of specific force equat ion) ,dynamic alignment(reinstalling the integral initial conditions of attitude matr ix differential equations), dynamic demarcation are realized, so that the performa nce of integrated navigation is improved. The experiment results show integrate d navigation system based on SINS/GPS/TACAN can gain better location accuracy.
Key words:  integrated navigation  federated filter  SINS  GPS  TACAN
安全联盟站长平台