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基于RT-LAB的组合导航仿真平台设计

张亚崇 岳亚洲 刘玉双 赵剡

张亚崇, 岳亚洲, 刘玉双, 等 . 基于RT-LAB的组合导航仿真平台设计[J]. 北京航空航天大学学报, 2013, 39(11): 1503-1508.
引用本文: 张亚崇, 岳亚洲, 刘玉双, 等 . 基于RT-LAB的组合导航仿真平台设计[J]. 北京航空航天大学学报, 2013, 39(11): 1503-1508.
Zhang Yachong, Yue Yazhou, Liu Yushuang, et al. Design of integrated navigation system simulation platform based on RT-LAB[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1503-1508. (in Chinese)
Citation: Zhang Yachong, Yue Yazhou, Liu Yushuang, et al. Design of integrated navigation system simulation platform based on RT-LAB[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1503-1508. (in Chinese)

基于RT-LAB的组合导航仿真平台设计

基金项目: 国家重点基础研究发展计划(973计划)资助项目(2010CB731800);航空科学基金资助项目(20100818018,20110818013)
详细信息
  • 中图分类号: V249.32;TP391.9

Design of integrated navigation system simulation platform based on RT-LAB

  • 摘要: 设计了一种基于RT-LAB的SINS/GPS/CNS(Strapdown Inertial Navigation System/Global Positioning System/Celestial Navigation System)组合导航系统仿真平台方案,建立具有故障检测、隔离和系统重构能力的基于联邦卡尔曼滤波器的姿态、位置、速度组合导航系统方案和结构.将SINS与GPS的位置之差和速度之差作为SINS/GPS子滤波器的观测量,通过CNS给出的载体惯性姿态信息获得SINS的姿态误差角测量信息.仿真结果表明,该系统方案具有较强的容错性能、较高的导航精度和很强的实时性能,为组合导航技术的研究提供了有益的参考.

     

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    [8] 刘宗玉, 陈明, 王伟.综合导航系统中的多级故障检测与隔离技术研究[J].中国空间科学技术, 2005, 2:48-52 Liu Zongyu, Chen Ming, Wang Wei.The study on multi-stage fault detection and isolation in integrated navigation system[J].Chinese Space Science and Technology, 2005, 2:48-52 (in Chinese)
    [9] 张亚崇, 陆志东, 雷宏杰.多传感器容错综合导航系统技术及其应用研究[J].弹箭与制导学报, 2009, 29 (4):51-54 Zhang Yachong, Lu Zhidong, Lei Hongjie.The research on techniques and application of multisensor fault-tolerant integrated navigation system[J].Journal of Projectiles, Rockets, Missiles and Guidance, 2009, 29 (4):51-54 (in Chinese)
    [10] 刘承香, 孙枫, 陈小刚, 等.野值存在情况下组合导航系统的容错技术研究[J].中国惯性技术学报, 2002, 10 (6):12-17 Liu Chengxiang, Sun Feng, Chen Xiaogang, et al.Fault tolerant on integrated navigation system when existing outliers[J].Journal of Chinese Inertial Technology, 2002, 10 (6):12-17 (in Chinese)
    [11] 杨峰, 程承, 张共愿, 等.一种亚轨道飞行器再入段组合导航方法[J].宇航学报, 2010, 31 (3):729-733 Yang Feng, Cheng Cheng, Zhang Gongyuan, et al.Simulation research of sub-orbital vehicle re-entry flight segment navigation technology[J].Journal of Astronautics, 2010, 31 (3):729-733 (in Chinese)
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出版历程
  • 收稿日期:  2012-12-04
  • 刊出日期:  2013-11-30

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