[1] Michael T, Timothy C, Jeremy R. Numerical skip entry guidance//Proceedings of the 29th Annual AAS Guidance and Control Conference, 2006.[2] Bairstow S H. Reentry guidance with extended range capability for low L/D spacecraft. Massachusetts: Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, 2006.[3] Vinh N X. Optimal trajectories in atmospheric flight[M]. New York: Elsevier, 1981: 190-213.[4] Vasile I. Optimal skip entry with terminal maximum velocity and heat constraint//Proceedings of the AIAA Atmospheric Flight Mechanics Conference and Exhibit, 1998.[5] Vasile I. Optimal profound entry into atmosphere with minimum heat and constraints//Proceedings of the AIAA Atmospheric Flight Mechanics Conference and Exhibit, 2001.[6] Zhou H, Zhou T, Chen W C, et al. Trajectory optimization in injection phase for hypersonic gliding vehicle[J]. Journal of Astronautics, 2006, 27(5): 44-49. (in Chinese) 周浩, 周韬, 陈万春, 等. 高超声速滑翔飞行器引入段弹道优化[J]. 宇航学报, 2006, 27(5): 44-49.[7] Wang Y, Lu Y P, Zhang C F. Skip-entry trajectory optimization design for lunar return vehicle with trim-flaps[J]. Journal of Astronautics, 2011, 32(2): 284-289. (in Chinese) 王银, 陆宇平, 张崇峰. 带配平翼月球返回舱跳跃再入轨迹优化设计[J]. 宇航学报, 2011, 32(2): 284-289.[8] Peng H J, Gao Q, Wu Z G, et al. Symplectic approaches for solving two-point boundary-value problems[J]. Journal of Guidance, Control, and Dynamics, 2012, 35(2): 653-658.[9] Hwang I, Li J H, Du D. Differential transformation and its application to nonlinear optimal control[J]. Journal of Dynamic Systems, Measurement, and Control, 2009, 131(5): 0510101-05101010.[10] John T B. Survey of numerical methods for trajectory optimization[J]. Journal of Guidance, Control, and Dynamics, 1998, 21(3): 653-658.[11] Tong K W, Zhou J P, He L S. Legendre-Gauss pseudospectral method for solving optimal control problem[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(6): 1531-1537. (in Chinese) 童科伟, 周建平, 何麟书. Legendre-Gauss 拟谱法求解最优控制问题[J]. 航空学报, 2008, 29(6): 1531-1537.[12] Fahroo F, Doman D B, Ngo A D. Modeling issues in footprint generation for reusable launch vehicles//Proceedings of the 2003 IEEE Aerospace Conference, 2005.[13] Fahroo F, Doman D B. A direct method for approach and landing trajectory reshaping with failure effect estimation//AIAA Guidance, Navigation, and Control Conference and Exhibit, 2005.[14] Bollino K, Ross I M, Doman D B. Six-degrees-of-freedom trajectory optimization for reusable launch vehicle footprint determination//Proceedings of AAS/AIAA Astrodynamics Specialists Conference, 2007.[15] Yong E M, Chen L, Tang G J. Trajectory optimization of hypersonic gliding reentry vehicle based on the physical programming[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(5): 1091-1097. (in Chinese) 雍恩米, 陈磊, 唐国金. 基于物理规划的高超声速飞行器滑翔式再入轨迹优化[J]. 航空学报, 2008, 29(5): 1091-1097.[16] Li J F, Chen W C. Numerical solution of optimal trajectory for hypersonic vehicle with constraints[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(9): 1605-1611. (in Chinese) 李佳峰, 陈万春. 带约束的高超声速飞行器最优弹道的数值算法[J]. 航空学报, 2009, 30(9): 1605-1611.[17] Stephen A W, Daniel W B, Benjamin M A, et al. Direct-entry, aerobraking and lifting aerocapture for human-rated lunar return vehicles//Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006.[18] Min X L, Pan T, Guo H L. Reentry trajectory optimization for manned deep space exploration[J]. Chinese Space Science and Technology, 2009(4): 8-12. (in Chinese) 闵学龙, 潘腾, 郭海林. 载人航天器深空飞行返回再入轨迹优化[J]. 中国空间科学技术, 2009(4): 8-12.[19] Lu P, Xue S B. Rapid generation of accurate entry landing footprints[J]. Journal of Guidance, Control, and Dynamics, 2010, 33(3): 756-767.[20] Christopher W B. Skip entry trajectory planning and guidance. Iowa: College of Engineering, Iowa State University, 2008. |