GUELMAN M. A qualitative study of proportional navigation [J]. IEEE Transactions on Aerospace and Electronic Systems, 1971, AES?7(4): 637-643.?
[2]
SONG S H, HA I J. A Lyapunov?like approach to performance analysis of 3-dimensional pure PNG laws [J]. IEEE Transactions on Aerospace and Electronic Systems, 1994, 30(1): 238-248.?
[3]
GHAWGHAWE S N, GHOSE D. Pure proportional navigation against time?varying target maneuvers [J]. IEEE Transactions on Aerospace and Electronic Systems, 1996, 32(4): 1336-1347.?
[4]
GUTMAN S. On optimal guidance for homing missiles [J]. Guidance and Control, 1979, 2(4): 296-300.?
[5]
ZHOU D, MU C D, XU W L. Adaptive sliding?mode guidance of a homing?missile [J]. Journal of Guidance, Control and Dynamics, 1999, 22(4): 589-594.?
[6]
MOON J, KIM K, KIM Y. Design of missile guidance law via variable structure control [J]. Journal of Guidance, Control, and Dynamics, 2001, 24(4): 659-664.?
[7]
POULTER R A, ANDERSON G M. A guidance concept for air?to?air missiles based on nonlinear differential game theory [C]// Proceedings of the National Aerospace and Electronics Conference. Dayton,USA, 1976.?
[8]
ANDERSON G M. Comparison of optimal control and differential game intercept missile guidance laws [J]. Journal of Guidance and Control, 1981, 4(2): 109-115.?
[9]
KUO C Y, SOETANTO D, CHIOU Y C. Geometric analysis of flight control command for tactical missile guidance [J]. IEEE Transactions on Control Systems Technology, 2001, 9(2): 234-243.?
[10]
LECHEVIN N, RABBATH C A. Lyapunov?based nonlinear missile guidance [J]. Guidance, 2004, 27(6): 1096-1102.