Research on load relief method for skip reentry of a lunar return vehicle

被引:0
|
作者
Guo, Min-Wen [1 ,2 ]
Wang, Da-Yi [1 ,2 ]
机构
[1] Beijing Institute of Control Engineering, Beijing 100190, China
[2] Science and Technology on Space Intelligent Control Laboratory, Beijing 100190, China
来源
Yuhang Xuebao/Journal of Astronautics | 2013年 / 34卷 / 12期
关键词
D O I
10.3873/j.issn.1000-1328.2013.12.005
中图分类号
学科分类号
摘要
引用
收藏
页码:1569 / 1577
相关论文
共 50 条
  • [1] Skip-reentry guidance, navigation, and control technology for the Chang'e-5 lunar-return vehicle
    Wang Y.
    Yang M.
    Yu D.
    Dong W.
    Wang Z.
    Xu Y.
    Zhongguo Kexue Jishu Kexue/Scientia Sinica Technologica, 2021, 51 (07): : 799 - 812
  • [2] Coupled Shape and Reentry Trajectory Optimization of Entry Vehicle for Lunar Return
    Wu, Xu Zhong
    Tang, Sheng Jing
    Guo, Jie
    MANUFACTURING ENGINEERING AND AUTOMATION II, PTS 1-3, 2012, 591-593 : 2624 - 2627
  • [3] Optimal Skip Entry Trajectory for Lunar Return Vehicle with Trim-Flaps
    Wang, Yin
    Yao, Keming
    MATHEMATICAL PROBLEMS IN ENGINEERING, 2017, 2017
  • [4] Skip-entry trajectory characteristic analysis and optimal design for lunar return vehicle
    Wang, Yin
    Lu, Yuping
    Zhang, Chongfeng
    Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics, 2010, 42 (01): : 21 - 24
  • [5] An investigation on combined entry guidance for lunar capsule skip reentry
    College of Aerospace Science and Engineering, National University of Defense Technology, Changsha
    410073, China
    Guofang Keji Daxue Xuebao, 6 (70-75):
  • [6] Skip Entry Trajectory Optimization of Lunar Return Vehicles
    Zhao J.-S.
    Wang J.-H.
    Wang B.-Q.
    Zhang J.-M.
    Zhu H.-B.
    Yuhang Xuebao/Journal of Astronautics, 2021, 42 (02): : 211 - 219
  • [7] Analysis and relief method of reentry aerodynamic load based on matched asymptotic expansions method
    Du Xin
    Li Hai-Yang
    ACTA PHYSICA SINICA, 2014, 63 (20)
  • [8] Electron Density Measurement in Reentry Shocks for Lunar Return
    Cruden, Brett A.
    JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2012, 26 (02) : 222 - 230
  • [9] Reentry trajectory optimization design for lunar return through coevolutionary algorithm
    School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
    不详
    Wang, F. (wangfengbohao@163.com), 1600, Beijing University of Aeronautics and Astronautics (BUAA) (40):
  • [10] Research on Reentry Vehicle Control Method Based on Robust Enhancement Strategy
    Liu Peicheng
    Ma Rong
    Li Xianqiang
    Pan Di
    2018 15TH INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION, ROBOTICS AND VISION (ICARCV), 2018, : 1192 - 1196