[1] Adler F P. Missile guidance by three-dimensional proportional navigation[J]. Journal of Applied Physics, 1956, 27(5): 500-507.[2] Yang C D, Yang C C. Analytical solution of three-dimensional realistic true proportional navigation[J]. Journal of Guidance, Control, and Dynamics, 1996, 19(3): 569-577.[3] Kim B S, Lee J G, Han H S. Biased PNG law for impact with angular constraint[J]. IEEE Transactions on Aerospace and Electronic Systems, 1998, 34(1): 277-288.[4] Ratnoo A, Ghose D. Impact angle constrained guidance against nonstationary nonmaneuvering targets[J]. Journal of Guidance, Control, and Dynamics, 2010, 33(1): 269-275.[5] Ratnoo A, Ghose D. Impact angle constrained interception of stationary targets[J]. Journal of Guidance, Control, and Dynamics, 2008, 31(6): 1816-1822.[6] Erer K S, Merttopcuoglu O. Indirect impact-angle-control against stationary targets using biased pure proportional navigation[J]. Journal of Guidance, Control, and Dynamics, 2012, 35(2): 700-704.[7] Shima T, Golan O M. Head pursuit guidance[J]. Journal of Guidance, Control, and Dynamics, 2007, 30(5): 1437-1444.[8] Shima T. Intercept-angle guidance[J]. Journal of Guidance, Control, and Dynamics, 2011, 34(2): 484-492.[9] Prasanna H M, Ghose D. Retro-proportional-navigation: a new guidance law for interception of high-speed targets[J]. Journal of Guidance, Control, and Dynamics, 2012, 35(2): 377-386.[10] Murtaugh S A, Criel H E. Fundamentals of proportional navigation[J]. IEEE Spectrum, 1966, 3(12): 75-85.[11] Brainin S, McGhee R. Optimal biased proportional navigation[J]. IEEE Transactions on Automatic Control, 1968, 13(4): 440-442.[12] Shukla U S, Mahapatra P R. Optimization of biased proportional navigation[J]. IEEE Transactions on Aerospace and Electronic Systems, 1989, 25(1): 73-79.[13] Jeong S K, Cho S J, Kim E G. Angle constraint biased PNG//5th Asian Control Conference. Piscataway: IEEE, 2004: 1849-1854.[14] Siouris G M. Missile guidance and control systems[M]. New York: Springer, 2004: 195-196.[15] Zarchan P. Tactical and strategic missile guidance[M]. 3rd ed. Reston: AIAA, 2002: 15.[16] Ulybyshev Y. Terminal guidance law based on proportional navigation[J]. Journal of Guidance, Control, and Dynamics, 2005, 28(4): 821-824.[17] Dou L, Dou J. Three-dimensional large landing angle guidance based on two-dimensional guidance laws[J]. Chinese Journal of Aeronautics, 2011, 24(6): 756-761.[18] Zheng L W, Jing W X, Gu L X. A terminal guidance law for exoatmospheric kill vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2007, 28(4): 953-958. (in Chinese) 郑立伟, 荆武兴, 谷立祥. 一种适用于大气层外动能拦截器的末制导律[J]. 航空学报, 2007, 28(4): 953-958.[19] Han D P, Sun W M, Zheng Z Q, et al. New three-dimensional guidance law based on Lie group method[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(3): 468-475. (in Chinese) 韩大鹏, 孙未蒙, 郑志强, 等. 一种基于李群方法的新型三维制导律设计[J]. 航空学报, 2009, 30(3): 468-475.[20] Peng S C, Sun W M, Wang N, et al. 3D guidance law of BTT missile considering movement coupling[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(5): 968-974. (in Chinese) 彭双春, 孙未蒙, 王楠, 等. 考虑运动耦合的BTT导弹三维制导律设计[J]. 航空学报, 2010, 31(5): 968-974.[21] Hu X J, Huang X M. Three-dimensional circular guidance law with impact angle constraints[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(3): 508-519. (in Chinese) 胡锡精, 黄雪梅. 具有碰撞角约束的三维圆轨迹制导律[J]. 航空学报, 2012, 33(3): 508-519.[22] Costello P. Simulink simulation of proportional navigation and command to line of sight missile guidance. California: Naval Postgraduate School, 1995. |