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 Jiaotong University(Science), 2019 , 24(5) : 671 -680 . DOI: 10.1007/s12204-019-2105-3

[1] BATTIN R H. Lambert’s problem revisited [J]. AIAAJournal, 1977, 15(5): 707-713. [2] BATTIN R H, VAUGHAN R M. An elegant Lambertalgorithm [J]. Journal of Guidance, Control, and Dynamics,1984, 7(6): 662-670. [3] VAUGHAN R M. An improvement of Gauss’ methodfor solving Lambert’s problem [D]. Massachusetts,USA: Massachusetts Institute of Technology, 1983. [4] DANCHICK R. Gauss meets Newton again: How tomake Gauss orbit determination from two position vectorsmore efficient and robust with Newton-Raphsoniterations [J]. Applied Mathematics and Computation,2008, 195(2): 364-375. [5] GOODYEAR W H. Completely general closed-formsolution for coordinates and partial derivatives of thetwo-body problems [J]. Astronomical Journal, 1965,70(3): 189-192. [6] BROOKS J E, LEMMON W W. A universal formulationfor conic trajectories: Basic variables and relationships[R]. Redondo Beach, CA, USA: Space TechnologyLabs., Inc., 1965. [7] BATTIN R H. An introduction to the mathematicsand methods of astrodynamics, revised edition [M].Reston, Virginia, USA: American Institute of Aeronauticsand Astronautics, Inc., 1999. [8] PRUSSING J E. A class of optimal two-impulserendezvous using multiple-revolution Lambert solutions[J]. Journal of the Astronautical Sciences, 2000,48(2/3): 131-148. [9] ZARCHAN P. Midcourse guidance strategiesfor exoatmospheric intercept [C]//Proceedings ofAIAA/BMDO Interceptor Technology Conference.Colorado Springs Colo, USA: AIAA, 1998: 1-11. [10] LIU S Y, WU R L, ZHOU B Z. Research on burnoutreference guidance law for an exo-atmospheric interceptor[J]. Aerospace Control, 2004, 22(2): 24-28 (inChinese). [11] NEWMAN B. Strategic intercept midcourse guidanceusing modified zero effort miss steering [J]. Journal ofGuidance, Control, and Dynamics, 1996, 19(1): 107-112. [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).