[1] 赵善友.防空导弹武器寻的制导控制系统设计[M].北京:中国宇航出版社,2005. ZHAO Shan-you.Design of Homing Guidance and Control system for Air Defense Missile Weapon[M].Beijing:China Astronautic Publishing House,2005. [2] 冯令兵,陈瑞华,雷泷杰.拦截大机动目标导弹制导优化设计[J].计算机仿真,2016,33(6):32-35. FENG Ling-bing,CHEN Rui-hua,LEI Long-jie.Design of Guidance Law for Intercept Missile with Trajectory Control Engine Intercepting Strongly Maneuvering Target[J].Computer Simulation,2016,33(6):32-35. [3] 刘宗源,高敏,王毅,等.二维弹道修正引信滚转角专家系统PID控制算法[J].现代防御技术,2019,47(2):24-29. LIU Zong-yuan,GAO Min,WANG Yi,et al.Pid Control Algorithm for Two-Dimensional Ballistic Modified Fuze Rolling Angle Expert System[J].Modern Defence Technology,2019,47(2):24-29. [4] 姜长生,孙隆和,吴庆宪,等.系统理论与鲁棒控制[M].北京:航空工业出版社,1998. JIANG Chang-sheng,SUN Long-he,WU Qing-xian,et al.System Theory and Robust Control[M].Beijing:Aviation Industry Publishing House,1998. [5] 袁耀,高庆丰.自寻的导弹制导回路等效时间常数估算方法[J].现代防御技术,2015,43(3):55-59. YUAN Yao,GAO Qing-feng. Estimation of Equivalent Time Constant for Self-Homing Missile Guidance Loop[J].Modern Defence Technology,2015,43(3):55-59. [6] P Zarchan.Tactical and Strategic Missile Guidance[M].1997. [7] Rafael Yanushevsky.现代导弹制导[M].薛丽华,范宇,宋闯,译.北京:国防工业出版社,2013. Rafael Yanushevsky.Modern Missile guidance[M].XUE Li-hua,FAN Yu,SONG Chuang,Translated.Beijing:National Defense Industry Press,2013. [8] BRYSON A E,HO Y C.Applied Optimal Control[M].Waltham,MA blaisdell,1969. [9] 候冰,张金鹏,曹有亮,等.抗目标大机动的制导指令校正算法研究[J].航空兵器,2018(2):29-33. HOU bing,ZHANG Jin-peng,CAO You-liang,et al.Study on Correction Proportional Guaidance Law Against High Maneuvering Target[J].Aero Weaponry,2018(2):29-33. [10] 安相宇,董朝阳,王青.一种基于EKF技术的天线罩瞄准误差补偿方法[J].系统仿真学报,2007,19(15):4099-4103. AN Xiang-yu,DONG Chao-yang,WANG Qing.Compensation Method based on EKF for Sloving Radome Error Slope[J].Journal of System Simulation,2007,19(15):4099-4103. [11] 李友年,江云,李世华,等.基于有限时间控制方法的三维空间导弹制导律设计[J].航空兵器,2016(3):26-29. LI You-nian,JIANG Yun,LI Shi-hua,et al.Three-Dimensional Guidance Laws for Missile based on Finite-time Control Method[J].Aero Weaponry,2016(3):26-29. [12] 赖超,王卫红,熊少锋.拦截大机动目标的三维制导控制一体化设计[J].宇航学报,2017,38(7):715-722. LAI Chao,WANG Wei-hong,XIONG Shao-feng.Integrated Guidance and Control Design Against Highly Maneuvering Target[J].Journal of Astronautics,2017,38(7):715-722. [13] 向哲,廖欣,黄书平,等.视线角加速度导引律分析及仿真应用研究[J].现代防御技术,2017,45(1):70-74. XIANG Zhe,LIAO Xin,HUANG Shu-ping,et al.Analysis of the Guiding Law of Line-of-Sight Acceleration and its Application in Dimulation[J].Modern Defence Technology,2017,45(1):70-74. [14] William Nesline F,Zarchan P.Radome Induced Miss Distance in Aerodynamically Controlled Homing Missle[J].AIAA,1984. [15] 任高峰,张拥军,张金鹏.基于捷联导引头测角信息的弹目相对位置估计方法[J].航空兵器,2015(4):8-11. REN Gao-feng,ZHANG Yong-jun,ZHANG Jin-peng.Estimation Method of Relative Position between Missile and Target with Bearing Measurement by Strapdown Seeker[J].Aero Weaponry,2015(4):8-11. |