[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).
|