Reentry trajectory design of low lift-to-drag ( L/D ) ratio spacecraft based on predictor-corrector method

[1] 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,1997:283-285 Zhao Hanyuan. The reentry dynamics and guidance of flying vehicles[M]. Changsha: National University of Defense Technology Press, 1997:283-285(in Chinese) [2] 王希季.航天器进入与返回技术[M].北京:宇航出版社,1991:114-120 Wang Xiji. Technology of space vehicle reentry and return [M].Beijing: China Astronautics Press House, 1991:114-120(in Chinese) [3] 戚发轫,朱仁璋,李颐黎.载人航天技术[M].北京:国防工业出版社, 2003:258-292 Qi Faren, Zhu Renzhang, Li Yili. Technology of manned astro-nautics[M]. Beijing: National Defense Industrial Press, 2003: 258-292(in Chinese) [4] 胡军.载人飞船全系数自适应再入升力控制[J].宇航学报,1998, 19(1):8-12 Hu Jun. All coefficients adaptive reentry lifting control of ma-nned spacecraft [J].Journal of Astronautics,1998, 19(1): 8-12(in Chinese) [5] 李季陆.载人飞船再入大气层航程控制的模糊控制器设计方法[J].航天控制,2001(1):23-30 Li Jilu. Fuzzy control design for range control in atmosphere re-entry of manned spacecraft[J]. Aeronautics Control,2001(1): 23- 30(in Chinese) [6] Rea J R, Putnam Z R. A comparison of two Orion skip entry guidance algorithms .AIAA-2007-6424, 2007 [7] Lu Ping. Predictor-Corrector entry guidance for low lifting vehicles . AIAA-2007-6425,2007 [8] Broome J M, Johnson Dr W. Orion entry, descent, and landing performance and mission design . AIAA-2007-6430, 2007 [9] Bairstow S H. Reentry guidance with extended range capability for low L/D spacecraft . Cambridge, Massachusetts: Department of Aeronautics and Astronautics, MIT, 2006 [10] 何力,赵汉元.载人飞船标准返回轨道设计[J].国防科技大学学报, 1996,18(3):63-67 He Li, Zhao Hanyuan. A design of standard return trajectory for manned spaceship[J]. Journal of National University of Defense Technology, 1996, 18(3):63-67(in Chinese)