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Article
Variable Coefficient Terminal-Phase Guidance Design for Deep Space High-Speed Impact
- ZHENG Huixin1,2, PENG Yuming1,2, WANG Wei1,2, XIE Pan1,2, LU Xi1,2, LI Haiyang1,2, CHEN Xiao1,2
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1. Shanghai Institute of Satellite Engineering, Shanghai 201109, China;
2. Shanghai Key Laboratory of Deep Space Exploration Technology, Shanghai 201109, China
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History
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Received |
Revised |
Published |
25 Dec 2020 |
13 Jul 2021 |
20 Oct 2021 |
Issue Date |
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20 Oct 2021 |
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References
[1] 马鹏斌, 宝音贺西. 近地小行星威胁与防御研究现状[J]. 深空探测学报(中英文),2016,3(1):10-17
MA P B, BAOYIN H X. Research status of the near-Earth asteroids' hazard and mitigation[J]. Journal of Deep Space Exploration,2016,3(1):10-17
[2] NASA. Near-Earth object survey and deflection analysis of alternatives, report to congress[R]. Washington, DC: NASA, 2007.
[3] WIE B. Dynamics and control of gravity tractor spacecraft for asteroid deflection[J]. Journal of Guidance, Control, and Dynamics,2008,31(5):1413-1423
[4] MILLER S D, STRAKA W C, BACHMEIER A S, et al. Earth-viewing satellite perspectives on the Chelyabinsk meteor event[J]. Proceedings of the National Academy of Sciences,2013,110(45):18092-18097
[5] 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
WANG Y M, LI M T. Orbital design and optimization of kinetic impactor for asteroid deflection[J]. Space Debris Research,2019,19(3):43-49
[6] 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):585-592
LI Y, CHEN H, LAN S W, et al. A method to improve interception efficiency in the defense against near-Earth asteroids[J]. Spacecraft Environmental Engineering,2017,34(6):585-592
[7] 韩柠, 刘辉, 王云财, 等. 基于比例导引的深空撞击脉冲导引律设计[J]. 动力学与控制学报,2019,17(1):86-90
HAN N, LIU H, WANG Y C, et al. Pulse guidance law for deep space impact base on the proportional guidance[J]. Journal of Dynamics and Control,2019,17(1):86-90
[8] RUSSEL C T. 深度撞击计划: 解密彗星之旅[M]. 陈小前, 蔡洪, 陈磊, 译. 北京: 国防工业出版社, 2008: 85- 86.
[9] WILLIAM H B. Deep impact mission design[J]. Space Science Reviews,2005,117(1-2):23-42
[10] 朱圣英, 崔平远, 崔祜涛. 小天体高速撞击器视线制导律设计[J]. 宇航学报,2010,31(2):373-379
ZHU S Y, CUI P Y, CUI G T. Design of line-of-sight guide law for small body high speed impactors[J]. Journal of Astronautics,2010,31(2):373-379
[11] 汤国建, 贾沛然. 运用比例导引实现对目标卫星的拦截[J]. 系统工程与电子技术,2001,23(2):25-27,64
TANG J G, JIA P R. Implementation of intercepting satellite by using proportional guidance[J]. Systems Engineering and Electronics,2001,23(2):25-27,64
[12] HAWKINS M, PITZ A, WIE B, et al. Terminal-phase guidance and control analysis of asteroid interceptors[C]// AIAA Guidance, Navigation, and Control Conference. [S. l.]: AIAA, 2013.
[13] ZARCHAN P. Tactical and strategic missile guidance[M]. Washington, DC: American Institute of Aeronautics and Astronautics, Inc. , 2012.
[14] 李雯雯, 姜长生. BTT导弹增广比例导引律研究[J]. 电光与控制,2008(10):16-20
LI W W, JIANG C S. Augmented proportional navigation guidance law for BTT missile[J]. Electronics Optics and Control,2008(10):16-20
[15] 周卫文, 梁晓庚, 贾晓洪. 小天体撞击末段脉冲比例制导律研究[J]. 电光与控制,2011(6):73-77
ZHOU W W, LIANG X G, JIA X H. End-stage guidance for impacting small asteroids using pulsed proportional guidance law[J]. Electronics Optics and Control,2011(6):73-77
[16] NEOys. latest published data [EB/OL]. (2018-11-24) [2021-07-13]. https://newton.spacedys.com/neodys/.
[17] SHAMPINE L F, REICHELT M W. The Matlab ODE suite[J]. SIAM Journal on Scientific Computing,1997,18:1-22