[1] Ren G F, Zhu S Y, Cui P Y, et al. Trajectory optimization for precision landing at Mars based on the Gaussian pseudospectral method[J]. Deep Space Exploration, 2011, 9(2): 1-7. (in Chinese) 任高峰, 朱圣英, 崔平远, 等. 基于高斯伪谱法的火星精确着陆轨迹优化方法研究[J]. 深空探测研究, 2011, 9(2): 1-7.[2] Rong W. Research on the deceleration and landing technology for Mars explorer[D]. Beijing: China Academy of Space Technology, 2008. (in Chinese) 荣伟. 火星探测器减速着陆技术研究[D]. 北京: 中国空间技术研究院, 2008.[3] Theisinger J E, Braun R D. Multi-objective hypersonic entry aeroshell shape optimization[J]. Journal of Spacecraft and Rockets, 2009, 46(5): 957-966.[4] Johnson J E. Aerothermodynamic optimization of Earth entry blunt-body heat shields for lunar and Mars return[D]. Washington, D, C.: University of Maryland, 2009.[5] Johnson J E, Starkey R P, Lewis M J. Aerothermodynamic optimization of reentry heat shield shapes for a crew exploration vehicle[J]. Journal of Spacecraft and Rockets, 2007, 44(4): 849-859.[6] Grant M J, Mendeck G F. Mars science laboratory entry optimization using particle swarm methodology[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit, 2007.[7] Ren G F, Cui P Y, Cui H T, et al. A new method of rapid trajectory optimization for Mars pin point landing[J]. Journal of Astronautics, 2013, 34(4): 464-472. (in Chinese) 任高峰, 崔平远, 崔祜涛, 等. 一种新型火星定点着陆轨迹快速优化方法[J]. 宇航学报, 2013, 34(4): 464-472.[8] Wang J, Pei H L, Wang N Z. Research on ablation for crew return vehicle based on re-entry trajectory and aerodynamic heating environment[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(1): 80-89. (in Chinese) 王俊, 裴海龙, 王乃洲. 基于再入轨迹和气动热环境的返回舱烧蚀研究[J]. 航空学报, 2014, 35(1): 80-89.[9] Hou L Q, Li H N, Huang F M, et al. A semi-analytical integrated model for capsule entering Mars atmosphere[J]. Journal of Astronautics, 2011, 32(11): 2312-2318. (in Chinese) 侯黎强, 李恒年, 黄福铭, 等. 一种半解析方法火星再入探测器一体化设计模型[J]. 宇航学报, 2011, 32(11): 2312-2318.[10] Deb K, Pratap A, Agrwal S, et al. A fast and elitist multiobjective genetic algorithm: NSGA-Ⅱ[J]. IEEE Transactions on Evolutionary Computation, 2002, 6(2): 182-197.[11] Zhang Q, Li H. MOEA/D: a multiobjective evolutionary algorithm based on decomposition[J]. IEEE Transactions on Evolutionary Computation, 2007, 11(6): 712-731.[12] Liu X, Lu H, Chen X. Optimization of navigation constellation by a multiobjective evolutionary algorithm based on decomposition[J]. Microcomputer Information, 2012, 28(9): 214-216. (in Chinese) 刘欣, 路辉, 陈晓. 基于分解思想的导航星座多目标优化[J]. 微计算机信息, 2012, 28(9): 214-216.[13] Fan P L, Yang T, Zhang X J. Multi-objective optimization of hypersonic test vehicle[J]. Journal of Astronautics, 2010, 31(4): 973-980. (in Chinese) 范培蕾, 杨涛, 张晓今. 高超声速试飞器系统的多目标优化设计[J]. 宇航学报, 2010, 31(4): 973-980.[14] Konstantinidis A, Yang K. Multi-objective energy-efficient dense deployment in wireless sensor networks using a hybrid problem-specific MOEA/D[J]. Applied Soft Computing, 2011, 11(6): 4117-4134.[15] Zhang Q B, Feng Z W, Liu Z M, et al. Fuel-time multiobjective optimal control of flexible structures based on MOEA/D[J]. Journal of National University of Defense Technology, 2009, 31(6): 73-76. (in Chinese) 张青斌, 丰志伟, 刘泽明, 等. 基于MOEA/D的柔性结构燃料-时间多目标优化控制研究[J]. 国防科技大学学报, 2009, 31(6): 73-76.[16] Zhang J D, Tang Q G, Zhang Q B, et al. The research on multiple-impulse correction submunition multi-objective optimization based on MOEA/D[J]. Journal of Projectiles, Rockets, Missile and Guidance, 2010, 30(2): 195-197. (in Chinese) 张建东, 唐乾刚, 张青斌, 等. 基于MOEA/D算法的多脉冲末修子弹多目标优化设计研究[J]. 弹箭与制导学报, 2010, 30(2): 195-197.[17] Desai P N, Knocke P C. Mars exploration rovers entry, descent, and landing trajectory analysis[J]. The Journal of the Astronautical Sciences, 2007, 55(3): 311-323.[18] Hankey W L, Elliott G A. Hypersonic lifting body optimization[J]. Journal of Spacecraft and Rockets, 1968, 5(12): 1463-1467.[19] Qu Z H, Liu W, Zeng M, et al. Hypersonic aerodynamics[M]. Changsha: Press of National University of Defense Technology, 2001: 19-21. (in Chinese) 翟章华, 刘伟, 曾明, 等. 高超声速空气动力学[M]. 长沙: 国防科技大学出版社, 2001: 19-21.[20] Thomas C. Aerodynamic validation using MER and phoenix entry flight data[D]. Raleigh: North Carolina State University, 2011.[21] Zhao H Y. Re-entry dynamics and guidance of flight vehicle[M]. Changsha: Press of National University of Defense Technology, 1997: 454. (in Chinese) 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: 454.[22] Sutton K, Graves R A. A general stagnation-point convective-heating equation for arbitrary gas mixtures. Washington, D.C.: NASA, 1971.[23] Shen H, Seywald H, Powell R W. Desensitizing the pin-point landing trajectory on Mars[C]//AIAA/AAS Astrodynamics Specialist Conference and Exhibit, 2008.[24] Deb K. Multi-objective optimization using evolutionary algorithms[M]. New York: Wiley, 2001.[25] Wells G, Braun R. Trajectory reconstruction of a Martian planetary probe mission: reconstruction of the Spirit Mars explorer rover entry, descent, and landing performance[C]//2nd International ARA Days, 2008. |