[1] Li S H, Pang D. Six key technologies of "returning home" safely[N]. China Aviation News, 2014-11-01(003) (in Chinese). 李淑姮, 庞丹. 安全"回家"之六大关键技术[N]. 中国航天报, 2014-11-01(003).
[2] Du X, Li H Y. Design of skip entry guidance for lunar-return vehicle[C]//Proceedings of Collection of the Eighth Academic Conference of Chinese Society of Astronautics Space Exploration Technology Committee. Beijing: Chinese Society of Astronautics, 2011: 33-36 (in Chinese). 杜昕, 李海阳. 探月飞船跳跃式再入制导律设计[C]//中国宇航学会深空探测技术专业委员会第八届学术年会论文集. 北京: 中国宇航学会, 2011: 33-36.
[3] Graves C A, Harpold J C. Apollo experience report-mission planning for Apollo entry, NASA TN D-6725[R]. Washington, D. C.: NASA, 1972.
[4] Lu P. Predictor-corrector entry guidance for low lifting vehicles[J]. Journal of Guidance, Control, and Dynamics, 2008, 31(4): 1067-1075.
[5] Kluever C A. Entry guidance using analytical atmospheric skip trajectories[J]. Journal of Guidance, Control, and Dynamics, 2008, 31(5): 1531-1534.
[6] Morth R. Reentry guidance for Apollo, MIT Instrumentation Lab Report R-532[R]. Cambridge, MA: Massachusetts Institute of Technology, 1966.
[7] Bairstow S H. Reentry guidance with extended range capability for low L/D spacecraft[D]. Cambridge, MA: Massachusetts Institute of Technology, 2006.
[8] Brunner C W, Lu P. Skip entry trajectory planning and guidance, AIAA-2007-6777[R]. Reston: AIAA, 2007.
[9] Lu P. Predictor-corrector entry guidance for law-lifting vehicles[J]. Journal of Guidance, Control, and Dynamics, 2008, 31(4): 1067-1075.
[10] Shi Y Y, Pottsepp L. Asymptotic expansion of a hypervelocity atmospheric entry problem[J]. AIAA Journal, 1969, 7(2): 353-355.
[11] Shi Y Y, Pottsepp L, Eckstein M C. A matched asymptotic solution for skipping entry into planetary atmosphere[J]. AIAA Journal, 1971, 9(4): 736-738.
[12] Vinh N X, Busemann A, Culp R D. Hypersonic and planetary entry flight mechanics[M]. Ann Arbor, MI: The University of Michigan Press, 1980: 254-272.
[13] Calise A J, Melamed N. Optimal guidance of aeroassisted transfer vehicles based on matched asymptotic expansions[J]. Journal of Guidance, Control, and Dynamics, 1995, 18(4): 709-717.
[14] Vinh N X. Optimal trajectories in atmospheric flight[M]. New York: Elsevier Scientific, 1981: 58-60.
[15] Liu R C. Some methods for singular perturbation problems[D]. Jilin: Jilin University, 2008 (in Chinese). 刘日成. 奇异摄动问题中的若干方法[D]. 吉林: 吉林大学, 2008.
[16] Xu B. Asymptotic analysis of solutions for some classes of singularly perturbed boundary value problems[D]. Maanshan: Anhui University of Technology, 2011 (in Chinese). 徐彪. 几类奇摄动边值问题解的渐进分析[D]. 马鞍山: 安徽工业大学, 2011.
[17] Kuo Z, Vinh N X. Improved matched asymptotic solutions for three-dimensional atmospheric skip trajectories[J]. Journal of Spacecraft and Rockets, 1997, 34(4): 496-502.
[18] Moseley P E. The Apollo entry guidance: A review of the mathematical development and its operational characteristics, Rept. 69-FMT-791[R]. Houston: TX, 1969. |