Predictive guidance method for the reentry vehicles based on fuzzy logic

[1] 任章,袁国雄.轨道武器战斗舱再入制导技术研究[J].航天控制,2005,23(2):4-7 Ren Zhang,Yuan Guoxiong.Study on reentry guidance technique for orbit weapon fighting cabin[J].Aerospace Control,2005,23(2):4-7(in Chinese) [2] 王俊波,田源,任章.基于最优化问题的混合再入制导方法[J].北京亚洲成人在线一二三四五六区学报,2009,36(6):736-470 Wang Junbo,Tian Yuan,Ren Zhang.Mixed guidance method for the reentry vehicles based on the optimization[J].Journal of Beijing University of Aeronautics and Astronautics,2009,36(6):736-470 [3] 胡正东,郭才发,蔡洪.天基对地打击动能武器再入解析预测制导技术[J].宇航学报,2009,30(3):1039-1044 Hu Zhengdong,Guo Caifa,Cai Hong.Analytical predictive guidance for space-to-ground kinetic weapon in reentry[J].Journal of Astronautics,2009,30(3):1039-1044(in Chinese) [4] 赵汉元.飞行器再入动力学和制导[M].长沙:国防科技大学出版社,1997:382-411 Zhao Hanyuan.Fight vehicle reentry dynamics and guidance[M].Changsha:National University of Defense Technology Press,1997:382-411( in Chinese) [5] Shen Zuojun,Lu Ping.On-board entry trajectory planning expanded to sub-orbital flight [R].AIAA-2003-5736,2003 [6] Hahn P V,Frederick R A,Slegers N.Predictive guidance of a projectile for hit-to-kill interception[J].Control Systems Technology, 2009,17(4):745-755