Journal of Shanghai Jiao Tong University (Science) ›› 2019, Vol. 24 ›› Issue (5): 671-680.doi: 10.1007/s12204-019-2105-3
• • 上一篇
DUAN Junhong (端军红), LIU Yuefeng (刘跃峰), WAN Kaifang (万开方)
出版日期:
2019-10-08
发布日期:
2019-09-27
通讯作者:
DUAN Junhong (端军红)
E-mail: duanjunhonggx@163.com
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
摘要: The intercept mode of space-based kinetic energy interceptor (KEI) is an essential problem to be solved in the concept design of KEI and is closely related to the KEI’s detailed designing and practical applications. However, this problem has not yet been investigated systematically and comprehensively. A suitable intercept mode for the KEI is proposed in this research. The intercept mode consists of three basic elements: the specific operation procedure, general scheme for the intercept trajectory, and mathematical model of the intercept mode. Numerical example is provided to demonstrate the feasibility and effectiveness of the intercept mode. The intercept mode proposed in this research is capable of achieving a rapid intercept, and is applicable to the universal space interception.
中图分类号:
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.
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.
[11] | NEWMAN B. Strategic intercept midcourse guidanceusing modified zero effort miss steering [J]. Journal ofGuidance, Control, and Dynamics, 1996, 19(1): 107-112. |
[1] | BATTIN R H. Lambert’s problem revisited [J]. AIAAJournal, 1977, 15(5): 707-713. |
[12] | TANG G J, JIA P R. Implementation of interceptingsatellite by using proportional guidance [J]. SystemsEngineering and Electronics, 2001, 23(2): 25-27 (inChinese). |
[2] | BATTIN R H, VAUGHAN R M. An elegant Lambertalgorithm [J]. Journal of Guidance, Control, and Dynamics,1984, 7(6): 662-670. |
[13] | ZES D. Exo-atmospheric intercept with J2 correction[C]//Guidance, Navigation, and Control Conferenceand Exhibit. Reston, Virginia, USA: AIAA, 1998:1061-1066. |
[3] | VAUGHAN R M. An improvement of Gauss’ methodfor solving Lambert’s problem [D]. Massachusetts,USA: Massachusetts Institute of Technology, 1983. |
[14] | MASSOUMNIA M A. Optimal midcourse guidancelaw for fixed-interval propulsive maneuvers [J]. Journalof Guidance, Control, and Dynamics, 1995, 18(3):465-470. |
[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. |
[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. |
[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. |
[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. |
[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. |
[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. |
[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. |
[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). |
[9] | ZARCHAN P. Midcourse guidance strategiesfor exoatmospheric intercept [C]//Proceedings ofAIAA/BMDO Interceptor Technology Conference.Colorado Springs Colo, USA: AIAA, 1998: 1-11. |
[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). |
[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). |
[22] | GAO X G, FAN H. Research on space-based antisatellitemode [J]. Fire Control and Command Control,2007, 32(8): 887-890 (in Chinese). |
[11] | NEWMAN B. Strategic intercept midcourse guidanceusing modified zero effort miss steering [J]. Journal ofGuidance, Control, and Dynamics, 1996, 19(1): 107-112. |
[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). |
[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). |
[1] | . [J]. J Shanghai Jiaotong Univ Sci, 2022, 27(6): 823-832. |
[2] | LIU Yueyang (刘岳洋), HU Qinglei (胡庆雷), GUO Lei (郭雷). Finite-Time Attitude Tracking Control of Spacecraft with Actuator Saturation[J]. Journal of Shanghai Jiao Tong University (Science), 2018, 23(5): 650-656. |
阅读次数 | ||||||
全文 |
|
|||||
摘要 |
|
|||||