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新型复合多视场光学敏感器及其导航方法

江洁 郑佳怡 凌思睿

江洁, 郑佳怡, 凌思睿等 . 新型复合多视场光学敏感器及其导航方法[J]. 北京航空航天大学学报, 2016, 42(1): 1-7. doi: 10.13700/j.bh.1001-5965.2015.0068
引用本文: 江洁, 郑佳怡, 凌思睿等 . 新型复合多视场光学敏感器及其导航方法[J]. 北京航空航天大学学报, 2016, 42(1): 1-7. doi: 10.13700/j.bh.1001-5965.2015.0068
JIANG Jie, ZHENG Jiayi, LING Siruiet al. A new composite multi-field-of-view optical sensor and its navigation method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(1): 1-7. doi: 10.13700/j.bh.1001-5965.2015.0068(in Chinese)
Citation: JIANG Jie, ZHENG Jiayi, LING Siruiet al. A new composite multi-field-of-view optical sensor and its navigation method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(1): 1-7. doi: 10.13700/j.bh.1001-5965.2015.0068(in Chinese)

新型复合多视场光学敏感器及其导航方法

doi: 10.13700/j.bh.1001-5965.2015.0068
基金项目: 国家自然科学基金(61222304);高等学校博士学科点专项科研基金(20121102110032)
详细信息
    作者简介:

    江洁女,博士,教授,博士生导师。主要研究方向:光电测试和光电导航。Tel.:010-82338497E-mail:jiangjie@buaa.edu.cn

    通讯作者:

    江洁,Tel.:010-82338497E-mail:jiangjie@buaa.edu.cn

  • 中图分类号: V448.22+4

A new composite multi-field-of-view optical sensor and its navigation method

Funds: National Natural Science Foundation of China (61222304);Specialized Research Fund for the Doctoral Program of Higher Education (20121102110032)
  • 摘要: 基于利用四面镜结构实现的复合多视场光学敏感器,给出了一种高精度天文导航方法,即通过四面镜同时观测地球、导航星和折射星,利用卫星、地球、恒星之间的位置关系,实现自主导航。通过研究导航量测信息的获取途径,给出了复合多视场光学敏感器的5种实用工作方式。结合卡尔曼滤波算法,建立了自主天文导航的仿真模型,并对5种工作方式进行了仿真与比较。仿真结果表明:双组直接敏感地平与单组间接敏感地平结合的导航方式精度最高,位置精度达到了10 m量级。

     

  • [1] KVHL C T F.Combined earth/star sensor for attitude and orbit determination of geostationary satellites[D].Stuttgart:University of Stuttgart,2005:27-79.
    [2] 宁晓琳,房建成.一种基于信息融合的卫星自主天文导航新方法[J].宇航学报,2003,24(6):579-583. NING X L,FANG J C.A new method of autonomous celestial navigation for spacecraft based on information fusion[J].Journal of Astronautics,2003,24(6):579-583(in Chinese).
    [3] 宁晓琳,马辛.地球卫星自主天文导航滤波方法性能分析[J].控制理论与应用,2010,27(4):423-430. NING X L,MA X.Analysis of filtering methods for satellite celestial navigation[J].Control Theory & Applications,2010,27(4):423-430(in Chinese).
    [4] 宋利芳,房建成.航天器天文导航中星敏感器最佳安装方位研究[J].北京航空航天大学学报,2006,32(1):22-26. SONG L F,FANG J C.Optimum installation azimuth of star sensor for spacecraft celestial navigation[J].Journal of Beijing University of Aeronautics and Astronautics,2006,32(1):22-26(in Chinese).
    [5] FANG J C,NING X L.Installation direction analysis of star sensors by hybrid condition number[J].IEEE Transactions on Instrumentation and Measurement,2009,58(10):3567-3582.
    [6] SAVELY R T,COCKRELL B F,PINES S.Apollo experience report onboard navigational and alignment software:NASA TN D-6471[R].Washington,D.C.:NASA,1972.
    [7] 田玉龙,房建成,宁晓琳.自主天文导航系统中的两种状态方程特性分析[J].系统工程与电子技术,2004,26(12):1829-1831. TIAN Y L,FANG J C,NING X L.Two kinds of motion equations used in autonomous celestial navigation and characteristic anslysis[J].Systems Engineering and Electronics,2004,26(12):1829-1831(in Chinese).
    [8] 房建成,宁晓琳.航天器自主天文导航原理与方法[M].北京:国防工业出版社,2006:103-107. FANG J C,NING X L.Spacecraft autonomous celestial navigation principle and method[M].Beijing:National Defense Industry Press,2006:103-107(in Chinese).
    [9] NING X L,WANG L H,BAI X B,et al.Autonomous satellite navigation using starlight refraction angle measurement[J].Advances in Space Research,2013,51(9):1761-1772.
    [10] 安笛.UKF性能分析及其在组合导航中的应用[D].哈尔滨:哈尔滨工程大学,2011:7-10. AN D.Performance analysis of UKF and application in integrated navigation system[D].Harbin:Harbin Engineering University,2011:7-10 (in Chinese).
    [11] 金智慧.近地卫星自主天文导航的算法与DSP实现研究[D].哈尔滨:哈尔滨工业大学,2007:19-26. JIN Z H.Study on autonomous celestial navigation algorithm and its DSP realization of near earth satellite[D].Harbin:Harbin Institute of Technology,2007:19-26 (in Chinese).
    [12] JULIER S J,UHLMANN J K.Reduced sigma point filters for the propagation of means and covariances through nonlinear transformations[C]//Proceedings of the American Control Conference.Piscataway,NJ:IEEE Press,2002,2:887-892.
    [13] JULIER S J,UHLMANN J K,DURRANT-WHYTE H F.A new method for the nonlinear transformation of means and covariances in filters and estimators[J].Transactions on Automatic Control,2000,45(3):477-482.
    [14] VAN DER MERWE R,WAN E A.The square-root unscented Kalman filter for state and parameter-estimation[C]//Proceedings of the IEEE International Conference on Acoustics,Speech,and Singnal Processing.Piscataway,NJ:IEEE Press,2001,6:3461-3464.
    [15] 陆海勇.捷联惯性导航系统中UKF滤波技术的应用研究[D].南京:南京航空航天大学,2009:25-29. LU H Y.Research on application of UKF in strapdown inertial navigation system[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2009:25-29(in Chinese).
    [16] 刘瑞华,刘建业.联邦滤波信息分配新方法[J].中国惯性技术学报,2001,9(2):28-32. LIU R H,LIU J Y.A New method of information-sharing in federated filter[J].Journal of Chinese Inertia Technology,2001,9(2):28-32(in Chinese).
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出版历程
  • 收稿日期:  2015-01-30
  • 网络出版日期:  2016-01-20

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