[1] CAI H,YANG Y,GEHLY S,et al.Improved tracklet association for space objects using short-arc optical measurements[J].Acta Astronautica,2018,151:836-847.
[2] PSIAKI M L,WEISMAN R M,JAH M K.Gaussian mixture approximation of angles-only initial orbit determination likelihood function[J].Journal of Guidance,Control,and Dynamics,2017,40(11):2807-2819.
[3] FUJIMOTO K,SCHEERES D J.Correlation of optical observations of earth-orbiting objects and initial orbit determination[J].Journal of guidance,control,and dynamics,2012,35(1):208-221.
[4] LI J,AN W,ZHOU Y.Initial orbit determination and correlation of the uncatalogued targets with too short arcs in space-based optical surveillance[J].Aerospace Science and Technology,2012,21(1):41-46.
[5] SCHUMACHER P W,GAEBLER J A,ROSCOE C W,et al.Parallel initial orbit determination using angles-only observation pairs[J].Celestial Mechanics and Dynamical Astronomy,2018,130(9):1-20.
[6] GRONCHI G F,DIMARE L,MILANI A.Orbit determination with the two-body integrals[J].Celestial Mechanics and Dynamical Astronomy,2010,107(3):299-318.
[7] GRONCHI G F,FARNOCCHIA D,DIMARE L.Orbit determination with the two-body integrals:Ii[J].Celestial Mechanics and Dynamical Astronomy,2011,110(3):257-270.
[8] GRONCHI G F,BAU G,MARO S.Orbit determination with the two-body integrals:ii[J].Celestial Mechanics and Dynamical Astronomy,2015,123(2):105-122.
[9] KARIMI R R,MORTARI D.Initial orbit determination using multiple observations[J].Celestial Mechanics and Dynamical Astronomy,2011,109(2):167-180.
[10] 刘林.关于初轨计算[J].飞行器测控学报,2004.23(3):41-50.
[11] 茅永兴.航天器轨道确定的单位矢量法[M].国防工业出版社,2009.
[12] 贾沛璋,吴连大.初轨计算的参考矢量法[J].天文学报,1997,38(4):353-358.
[13] 戎鹏志,陆本魁.一种改进型的Laplace轨道计算方法[J].天文学报,1991,32(1):62-72.
[14] 甘庆波.一种基于星间方向观测的初轨计算方法[J].宇航学报,2007,28(3):619-622.
[15] SOKOLSKAYA M J.On the Laplacian orbit determination of asteroids[J].Plane t.Space Scz.,1997,45(12):1575-1580.
[16] 李艳斌.改进的Laplace算法初轨计算的收敛问题[J].无线电通信技术,1998,24(2):57-61.
[17] 陆本魁,李剑峰.一种有摄初轨计算的单位矢量法[J].宇航学报,1999,20(1):14-20.
[18] 陆本魁,戎鹏志,吴建民,等.人造地球卫星初轨计算的单位矢量法[J].宇航学报,1997,18(2):1-7.
[19] LU B K,MA J Y,XIA Y,et al.A method of initial orbit determination for long arc data[J].Acta Astmn.Sic.2004,28:88-93.
[20] GOODING R.A new procedure for the solution of the classical problem of minimal orbit determination from three lines of sight[J].Celestial Mechanics and Dynamical Astronomy,1996,66(4):387-423.
[21] 闰瑞东,王荣兰,龚建村,等.基于Gooding算法的天基光学目标跟踪定轨[J].空间科学学报,2021.
[22] 刘光明.基于连续同伦算法的天基仅测角初定轨方法[J].飞行器测控学报,2015,34(5):6.
[23] 李庆扬.非线性方程组数值解法[M].非线性方程组数值解法,1987.
[24] 宋叶志,邵瑞,王蕾,等.低轨星载光学测量确定静止卫星轨道的方法[J].航天返回与遥感,2021(042-001).
[25] KARIMI R R,MORTARI D.Orbit determination using prescribed orbits[C].AAS/AIAA Space Flight Mechanics Meeting Conference.2010:2010-236.
[26] KARIMI R R,MORTARI D.A performance based comparison of angle-only initial orbit determination methods[J].Adv.Astronaut.Sci.,AAS/AIAA,Hilton Head Island,South Carolina,2013,150:1793-1809.
[27] 王志胜,周军,王道波.基于角度量观测的卫星初轨计算技术研究[J].弹箭与制导学报,2002,22(4):190-193.
[28] VITARIUS P J,HAHS D,GREGORY D A.A Keplerian approach to angles-only orbit determination[J].Proc.SPlE,2006,6220:6220M1-7.
[29] MILANI A,GRONCHI G F,KNEZEVI Z,et al.Orbit determination with very short arcs II.Identi-fications[J].Icarus,2005(179):350-374.
[30] VIRTANEN J,FEDORETS G,GRANVIK M,et al.Statistical ranging of asteroid orbits:efficient MCMC and importance samplers[J].IAU General Assembly,2015,22:56438.
[31] JAGGI A,BEUTLER G,HUGENTOBLER U.Reduced-dynamic orbit determination and the use of accelerometer data[J].Adv.Space Res.2005,36:438-444.
[32] YOSHIKAWAA M,KAWAGUCHIA J,YAMAKAWA H,et al.Summary of the orbit determination of NOZOMI spacecraft for all the mission period[J].Acta Astronautica,2005,57:510-519.
[33] LIU L,LIU Y C.Precise orbit determination for lunar satellite[J].Acta Astronautica.2002,51(1-9):501-506.
[34] ROMERO I,GARCIA C,KAHLE R,et al.Precise orbit determination of GLONASS satellites at the European space agency[J].Adv.& ace Res,2002,30(2):281-287.
[35] 王宜举,修乃华.非线性最优化理论与方法[M].北京:科学出版社,2013.
[36] 研仔文训,谢金星.现代优化计算方法[M].北京:清华大学出版社,2005.
[37] VIRTANEN J,FEDORETS G,GRANVIK M,et al.Statistical ranging of asteroid orbits:efficient MCMC and importance samplers[J].IAU General Assembly,2015,22:56438.
[38] KALMAN R E.New methods in wiener filtering theory[C].Proceedings of the First Symposium on Engineering Applications of Random Function Theory and Probability,John Wiley&Sons,New York.1963.
[39] BUCY R S,JOSEPH P D.Filtering for stochastic processes with applications[M].New York:Guidance Interscience Publishers,John Wiley&Sons 1968.
[40] STEVEN M K.Fundamentals of statistical signal processing volume I estimation theory[M].Pearson Education,Inc,1993.
[41] AIDALA V J,NARDONA S C.Biased estimation properties of the pseudolinear tracking filter[J].IEEE Transactions on Aerospace and Electronic Systems,1982,18(4):432-441.
[42] AIDALA V J,HAMMEL S E.Utilization of modified polar coordinates for bearings-only tracking[J].IEEE Transaction on Automatic Control,1983,28(3):283-294.
[43] SONG L T,SPEYER J A.Filter with application to stochastic analysis of a modified gain extend kalman estimation with bearings only measurements[J].IEEE Transaction on Automatic Control,1985,30(10):940-949.
[44] FAGIN S L.Comments On “a Method for Improving Extended Kalman Filter Performance for Angle-Only Passive Ranging”[J].IEEE Transactions on Aerospace and Electronic Systems,1995,31(3):1148-1150.
[45] 郭福成,李宗华,孙仲康.无源定位跟踪中修正协方差扩展卡尔曼滤波算法[J].电子与信息学报,2004,26(6):917-922.
[46] 潘泉,杨峰,叶亮,等.一类非线性滤波器一UKF综述[J].控制与决策,2005,20(5):481-489.
[47] JULIER S J,UHLMANN J K.Unscented filtering and nonlinear estimation[J].Proceedings of the IEEE,2004,92(3):401-422.
[48] CHANG G.Kalman filter with both adaptivity and robustness[J].Process Contro1,2014,24(3):81-87.
[49] CHANG L,HU B,LI A,et al.Transformed unscented Kalman filter[J].IEEE Transactions on Autom
[50] -atic Control,2013,58(1):252-257.
[51] HORWOOD J T,POORE A B.Adaptive Gaussian sum filters for space surveillance[J].IEEE Transactions on Automatic Control,2011,56(8):1777-1790.
[52] HUR H,AHN H S.Discrete time filtering for mobile robot localization using wireless sensor network[J].IEEE Sensors Journa1,2013,13(1):245-252.
[53] 王正明,朱炬波.弹道跟踪数据的节省参数模型及应用[J].中国科学E辑,1999,29(2):146-154.
[54] 赵德勇.卫星联合定轨的参数化信息融合技术及应用[D].国防科技大学博士学位论文,2007.
[55] 朱珺.一种基于信息融合的空间目标高精度定轨方法[J].电子测量技术,2013,36(9):41-44.
[56] 刘也,朱炬波,等.基于滑动多项式表示弹道的测迷定轨算法[J].弹道学报,2008,20(2):73-76.
[57] 淡鹏,李恒年,等.基于多元非完备信息的实时滤波定轨方法[J].宇航动力学学报,2013,3(2):37-40.