Research of missile random maneuver strategy

[1] Zarchan P. Proportional navigation and weaving targets[J].Journal of Guidance Control and Dynamics,1995,18(5):969~974 [2]Ohlmeyer E J. Root-mean-square miss distance of proportional navigation missile against sinusoidal target[J]. Journal of Guidance Control and Dynamics, 1996, 19(3):563~568 [3]Takehira T. Analytical solution of missile terminal guidance [J]. Journal of Guidance Control and Dynamics,1998,21(2):342~348 [4] 姜玉宪,崔 静. 导弹摆动式突防策略的有效性[J]. 北京航空航天大学学报,2002,28(2):133~136 Jiang Yuxian,Cui Jing.Effectiveness of weaving maneuver stratety of a missile .Jorunal of Beijing University of Aeronautics and Astronautics,2002, 28(2):133~136(in Chinese) [5] Zarchan P. Tactical and strategic missile guidance[M]. Washington DC:AIAA Inc,1990 [6]Shinar J, Steinberg D. Analysis of optimal evasive maneuvers based on a linearized two-dimension kinematics model [J]. Journal of Aircraft, 1977,14(8):795~801 [7]Forte I, Shinar J. Can a mixed guidance strategy improve missile performance [J]. Journal of Aircraft, 1988,25(1):53~58 [8] 姜玉宪. 控制系统仿真[M]. 北京:北京航空航天大学出版社,1998.84~115 Jiang Yuxian. Simulink of control system[M]. Beijing:Beijing University of Aeronautics and Astronautics Press, 1998.84~115(in Chinese)