[1] |
MULDOON A, ELKAIM G, WEEDEN B, et al. Improved orbital debris trajectory estimation based on sequential TLE Processing[C]//60th International Astronautical Congress. Daejeon, Korea, 2009
|
[2] |
VALLADO D A. Fundamentals of Astrodynamics and Applications[M]. 4th ed. California: Microcosm Press, 2013
|
[3] |
LIDTKE A A, GONDELACH D J, ARMELLIN R. Optimising filtering of two-line element sets to increase re-entry prediction accuracy for GTO objects[J]. Advances in Space Research, 2019, 63(3): 1289-1317 doi: 10.1016/j.asr.2018.10.018
|
[4] |
OSWEILER V P. Covariance Estimation and Autocorrelation of NORAD Two-Line Element Sets[D]. Wright-Patterso: Air Force Institute of Technology, 2006
|
[5] |
LEGENDRE P, DEGUINE B, GARMIER R, et al. Two line element accuracy assessment based on a mixture of Gaussian laws[C]//AIAA/AAS Astrodynamics Specialist Conference and Exhibit. Keystone, Colorado: AIAA, 2006: 6518
|
[6] |
VALLADO D A, CEFOLA P J. Two-line element sets-Practice and use[C]//63rd International Astronautical Congress. Naples, Italy: International Astronautical Federation, 2012: 29-44
|
[7] |
SAUNDERS A, SWINERD G G, LEWIS H G. Deriving accurate satellite ballistic coefficients from two-line element data[J]. Journal of Spacecraft and Rockets, 2012, 49(1): 175-184 doi: 10.2514/1.A32023
|
[8] |
GEUL J, MOOIJ E, NOOMEN R. GOCE statistical re-entry predictions[C]//Proceedings of 7th European Conference on Space Debris. Darmstadt, Germany: The ESA Space Debris Office, 2017
|
[9] |
SONG W D, WANG R L, WANG J. A simple and valid analysis method for orbit anomaly detection[J]. Advances in Space Research, 2012, 49(2): 386-391 doi: 10.1016/j.asr.2011.10.007
|
[10] |
GONDELACH D, LIDTKE A A, ARMELLIN R, et al. Re-entry prediction of spent rocket bodies in GTO[C]//26th AAS/AIAA Space Flight Mechanics Meeting. 2016
|
[11] |
ÁGUEDA A, AIVAR L, TIRADO J, et al. In-orbit lifetime prediction for LEO and HEO based on orbit determination from TLE data[C]//6th European Conference on Space Debris. Darmstadt, Germany, 2013: 22-25
|
[12] |
DOLADO J C, AIVAR-GARCIA L, MATÉ A A, et al. OPERA: a tool for lifetime prediction based on orbit determination from TLE data[C]//24th International Symposium on Space Flight Dynamics. Laurel, MD, USA, 2004
|
[13] |
PATERA R P. Space event detection method[J]. Journal of Spacecraft and Rockets, 2008, 45(3): 554-559 doi: 10.2514/1.30348
|
[14] |
LIU J H, LIU L, DU J L, et al. TLE outlier detection based on expectation maximization algorithm[J]. Advances in Space Research, 2021, 68(7): 2695-2712 doi: 10.1016/j.asr.2021.07.013
|
[15] |
崔希璋, 於宗俦, 陶本藻, 等. 广义测量平差[M]. 2版. 武汉: 武汉大学出版社, 2009CUI Xizhang, YU Zongchou, TAO Benzao, et al. Generalized Survey Adjustment[M]. 2nd ed. Wuhan: Wuhan University Press, 2009
|
[16] |
刘劲宏. 基于TLE数据的空间目标大气再入预报[D]. 武汉: 武汉大学, 2020LIU Jinghong. Prediction of Atmospheric Reentry of Space Objects Based on TLE Data[D]. Wuhan: Wuhan University, 2020
|