[1] 龚自正,李明,陈川,等.小行星监测预警、安全防御和资源利用的前沿科学问题及关键技术[J].科学通报,2020,65:346—372.
[2] CNEOS Discovery Statistics web page[EB/OL].https://cneos.jpl.nasa.gov/stats/,2021-04-17.
[3] 柳森,党雷宁,赵君尧,等.小行星撞击地球的超高速问题[J].力学学报,2018,50(06):37—53.
[4] Vasilyev NV.The tunguska meteorite problem today[J].Planetary andSpace Science,1998,46(2-3):129—150.
[5] Popova OP,Jenniskens P,Emel'yanenko V,et al.Chelyabinsk airburst,damage assessment,meteorite recovery and characterization[J].Science,2013,342(6162):1069—1073.
[6] Gupta S C,Ahrens T J,Yang WB.Shock induced vaporization of anhydrite and global cooling from the KT impact[J].Earth and Planetary Science Letters,2001,188(34):399—412.
[7] Koschny D,Busch M,Drolshagen G.Asteroid observations at the Optical Ground Station in 2010-Lessons learnt[J].Acta Astronaut,2010,90:49—55.
[8] D Laurin,Hildebrand A,Cardinal R,et al.NEOSSat:a Canadian small space telescope for near Earth asteroid detection[J].Proc Spie,2008,7010:34.
[9] Sanchez J P,Colombo C,Vasile M,et al.Multicriteria comparison among several mitigation strategies for dangerous near-Earth objects[J].Journal of Guidance Control & Dynamics,2009,32(1):121—142.
[10] Thiry N,Vasile M.Statistical multi-criteria evaluation of non-nuclear asteroid deflection methods[J].Acta Astronautica,2017,140.
[11] Motiwala SA,Mathias DL,Mattenberger CJ.An integrated physics-based risk model for assessing the asteroid threat[C] //InternationalTopical Meeting on Probabilistic Safety Assessment and Analysis,Idaho,USA,2015.
[12] Collins G S,Melosh H J,Marcus RA.Earth impact effects program:a web-based computer program for calculating the regional environmental consequences of a meteoroid impact on earth.Meteoritics & Planetary Science,2005,40(6):817—840.
[13] Mathias D L,Wheeler L F,Dotson J L.A probabilistic asteroid impact risk model :assessment of sub-300 m impacts[J].Icarus,2017,289:106—119.
[14] JA González,M Belló,JF Martín-Albo,et al.Don Quijote:An ESA mission for the assessment of the NEO threat[C] //55th International Astronautical Congress,Vancouver,Canada 2004.
[15] Harris A W,Barucci M A,Cano J L,et al.The European Union funded NEOShield project:A global approach to near-Earth object impact threat mitigation[J].Acta Astronautica,2013,90(1):80—84.
[16] Carnelli I,Atchison,et al.Asteroid impact and deflection assessment mission[J].Acta astronautica,2015,115:262—269.
[17] 张韵,刘岩,李俊峰.小行星防御动能撞击效果评估[J].深空探测学报,2017,4(1):51—57.
[18] 张飞.小行星防御中的撞击研究[D].博士学位论文.南京:南京大学,2018.
[19] 姜宇,程彬,宝音贺西,等.潜在威胁小行星碰撞防御的计算与分析[J].深空探测学报,2017,4(2):190—195.
[20] 王艺睿,李明涛.动能撞击小行星防御轨道优化设计[J].空间碎片研究,2019,19(3):43—49.
[21] 丁文哲,杨虹,陈峰.基于高斯算法的小行星固定时间拦截[J].兵器装备工程学报,2016(3):106—110.
[22] 李毅,陈鸿,兰胜威,等.一种提升近地小行星防御中拦截效率的方法[J].航天器环境工程,2017,34 (6):19—26.
[23] 陈川.激光驱动移除空间碎片动力学行为及应用研究[D].博士学位论文.北京:中国空间技术研究院,2018.
[24] 邬静云.太阳帆绳系小行星动力学与控制研究[D].硕士学位论文.南京:南京航空航天大学,2016.
[25] Li Mingtao,Wang Yirui,Wang Youliang,et al.Enhanced kinetic impactor for deflecting large potentially hazardous asteroids via maneuvering space rocks[J].Scientific Reports,2020,10(1).
[26] Wang Yirui,Li Mingtao,Gong Zizheng,et al.Assembled kinetic impactor for deflecting asteroids by combining the spacecraft with the launch vehicle upper stage[J].Icarus,2021,368:114596.
[27] NASAGlenn Research Center Space Science Projects Office.LTTT Suite Optimization Tools,in:A.Timothy Reckart (Ed.),,23 April 2012.[EB/OL].http://microgravity.grc.nasa.gov/SSPO/ISPTProg/LTTT/〉,2012-05.
[28] General Mission Analysis Tool (GMAT),National Aeronautics and Space Administration Goddard Space Flight Center.[EB/OL].http://gmat.gsfc.nasa.gov/index.html〉,2012-05.
[29] Vardaxis G,Pitz A,Wie B.Conceptual design of planetary defense technology demonstration mission,AAS 12 128,AAS/AIAA Space Flight Mechanics Meeting,Charleston,SC,2012.
[30] Kaplinger B D.Physical modeling and high-performance GPU computing for characterization,interception,and disruption of hazardous near-Earth objects[D].Doctor Dissertation,Ames:Iowa State University,2013.
[31] Melamed N.Development of a handbook and an on-line tool on defending Earth against Potentially Hazardous Objects[J].Acta Astronautica,2013,90(1):165—172.
[32] Vardaxis G,Wie B.Near-Earth object intercept trajectory design for planetary defense[J].Acta Astronautica,2014,101(AUG.-SEP.):1—15.
[33] Vardaxis G,Wie B.Development of an asteroid mission design software tool for planetary defense[C] //3rd Planetary Defense Conference,Flagstaff,USA,2013.
[34] Cano J L,Bellei G,J Martín.NEO Threat mitigation software tools within the NEO Shield project and application to 2015 PDC[C] //4th IAA Planetary Defense Conference-PDC 2015.Frascati,Roma,Italy,2015.
[35] Cano J L,Bellei G,J Martín.Integrated END-TO-END NEO threat mitigation software suite[C] //64th International Astronautical Congress,Beijing,China,2013.