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基于SAR辅助的惯导/星光组合导航系统研究
引用本文:韩龄,熊智,于永军,刘建业.基于SAR辅助的惯导/星光组合导航系统研究[J].传感器与微系统,2011,30(7):16-19.
作者姓名:韩龄  熊智  于永军  刘建业
作者单位:南京航空航天大学导航研究中心,江苏南京,210016
基金项目:国家自然科学基金资助项目(60904091); 航空科学基金资助项目(20090852012)
摘    要:针对高空、长航时无人飞行器在对地观测成像期间对导航自主性和高精度的需求,研究了基于SAR辅助的惯导/星光姿态组合导航系统.针对SAR图像导航输出的间断性和多传感器组合导航系统中量测输出的不同步特性,设计了解决非连续性量测修正的多传感器组合导航滤波器模型.提出了解决多传感器量测不同步问题的异步集中滤波算法.仿真结果表明:...

关 键 词:星光导航  惯性导航  合成孔径雷达  量测不同步  集中卡尔曼滤波

Research on INS/star integrated navigation system aided by SAR
HAN Ling,XIONG Zhi,YU Yong-jun,LIU Jian-ye.Research on INS/star integrated navigation system aided by SAR[J].Transducer and Microsystem Technology,2011,30(7):16-19.
Authors:HAN Ling  XIONG Zhi  YU Yong-jun  LIU Jian-ye
Affiliation:HAN Ling,XIONG Zhi,YU Yong-jun,LIU Jian-ye(Nanjing University of Aeronautics and Astronautics,Navigation Research Center,Nanjing 210016,China)
Abstract:Considering that the HALE UAV has high requirement to the autonomous navigation performance and precision during the imaging,the INS/star attitude integrated navigation system aided by the SAR is researched.Combining the disconnected output characteristic of the SAR image navigation and the asynchronous characteristic of the multi-sensor integrated navigation system,the multi-sensor integrated navigation filter model is designed which is applied to solve the discontinuous measurement modified value.The uneq...
Keywords:star navigation  inertial navigation  SAR  asynchronous measurement  aggregated Kalman filtering  
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