Journal of Shanghai Jiao Tong University (Science) ›› 2019, Vol. 24 ›› Issue (5): 671-680.doi: 10.1007/s12204-019-2105-3
DUAN Junhong (端军红), LIU Yuefeng (刘跃峰), WAN Kaifang (万开方)
Online:
2019-10-08
Published:
2019-09-27
Contact:
DUAN Junhong (端军红)
E-mail: duanjunhonggx@163.com
CLC Number:
DUAN Junhong (端军红), LIU Yuefeng (刘跃峰), WAN Kaifang (万开方) . Intercept Mode Suitable for the Space-Based Kinetic Energy Interceptor[J]. Journal of Shanghai Jiao Tong University (Science), 2019, 24(5): 671-680.
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[12] | TANG G J, JIA P R. Implementation of interceptingsatellite by using proportional guidance [J]. SystemsEngineering and Electronics, 2001, 23(2): 25-27 (inChinese). |
[13] | ZES D. Exo-atmospheric intercept with J2 correction[C]//Guidance, Navigation, and Control Conferenceand Exhibit. Reston, Virginia, USA: AIAA, 1998:1061-1066. |
[14] | MASSOUMNIA M A. Optimal midcourse guidancelaw for fixed-interval propulsive maneuvers [J]. Journalof Guidance, Control, and Dynamics, 1995, 18(3):465-470. |
[15] | SONG E J, TAHK M J. Three-dimensional midcourseguidance using neural networks for interception of ballistictargets [J]. IEEE Transactions on Aerospace andElectronic Systems, 2002, 38(2): 404-414. |
[16] | GE L Z, SHEN Y, GAO Y F, et al. Head pursuitvariable structure guidance law for three-dimensionalspace interception [J]. Chinese Journal of Aeronautics,2008, 21(3): 247-251. |
[17] | LAM V C. Acceleration-compensated zero-effort-missguidance law [J]. Journal of Guidance, Control, andDynamics, 2007, 30(4): 1159-1162. |
[18] | EBRAHIMI B, BAHRAMI M, ROSHANIAN J. Optimalsliding-mode guidance with terminal velocity constraintfor fixed-interval propulsive maneuvers [J]. ActaAstronautica, 2008, 62(10/11): 556-562. |
[19] | JONER S, QUINQUIS I. Control of an exoatmospherickill vehicle with a solid propulsion attitude control system[C]//Proceedings of the AIAA Guidance, Navigation,and Control Conference and Exhibit. Massachusetts,USA: AIAA, 2006: 1-10. |
[20] | DUAN J H, GAO X G. Design of the on-off controllaws of kinetic kill vehicle’s attitude and orbit controlthrustors [J]. Flight Dynamics, 2010, 28(1): 57-60 (inChinese). |
[21] | LIU S Y, WU R L, ZHOU B Z. An on-off control lawof a divert thruster for an exoatmospheric interceptorduring its terminal course [J]. Journal of Astronautics,2005, 26(suppl): 106-109 (in Chinese). |
[22] | GAO X G, FAN H. Research on space-based antisatellitemode [J]. Fire Control and Command Control,2007, 32(8): 887-890 (in Chinese). |
[23] | DUAN J H, GAO X G. An orbit maneuver strategy forthe satellite based on evaluating the pregnable area ofincoming kinetic kill vehicle [J]. Journal of Astronautics,2011, 32(9): 1953-1962 (in Chinese). |
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