首页 | 本学科首页   官方微博 | 高级检索  
     

无地面基准的相对导航系统设计与仿真
引用本文:秦红磊,王莉,丛丽.无地面基准的相对导航系统设计与仿真[J].计算机工程与设计,2012,33(4):1504-1508.
作者姓名:秦红磊  王莉  丛丽
作者单位:北京航空航天大学电子信息工程学院,北京,100191
基金项目:国家973重点基础研究发展计划基金项目(2010CB731805)
摘    要:在无地面基准的机群编队飞行JTIDS/INS组合导航系统中,采用新的相对坐标系建立方法克服了绝对位置偏差对相对导航定位精度的影响,同时在原有的TOA观测量的基础上增加了DOA观测量,采用UKF非线性滤波算法进行系统滤波器设计,进一步提高了相对定位精度,并设计了JTIDS/INS组合导航仿真软件平台.仿真结果表明,该方法在收敛速度和定位精度方面都有很好的性能.

关 键 词:联合战术分发系统  相对导航  到达时间  到达方向  惯导系统  组合导航  无轨迹卡尔曼滤波  仿真平台

Design and simulation of relative navigation system without geographical position reference (GPR)
QIN Hong-lei , WANG Li , CONG Li.Design and simulation of relative navigation system without geographical position reference (GPR)[J].Computer Engineering and Design,2012,33(4):1504-1508.
Authors:QIN Hong-lei  WANG Li  CONG Li
Affiliation:(School of Electronic Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China)
Abstract:In JTIDS/INS integrated navigation system without geographical position reference(GPR) for aircraft formation flying,a new relative coordinate establishing method is proposed to overcome the affect of the absolute position error.Based on original TOA observation,the DOA observation is introduced.In order to further improve the relative position accuracy,the unscented Kalman filter algorithm is adopted for system filter design.Then the JTIDS/INS integrated navigation system simulation platform is designed.The simulation result shows that the proposed method perform well in convergence and position accuracy.
Keywords:JTIDS  relative navigation  TOA  DOA  INS  integrated navigation  UKF  simulation platform
本文献已被 CNKI 万方数据 等数据库收录!
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