Prediction and Validation of Landing Stability of a Lunar Lander by a Classification Map Based on Touchdown Landing Dynamics' Simulation Considering Soft Ground

被引:9
|
作者
Kim, Yeong-Bae [1 ]
Jeong, Hyun-Jae [2 ]
Park, Shin-Mu [3 ]
Lim, Jae Hyuk [1 ]
Lee, Hoon-Hee [3 ]
机构
[1] Jeonbuk Natl Univ, Div Mech Engn, 567 Baekje Daero, Jeonju Si 54896, South Korea
[2] Agcy Def Dev, 160,Bugyuseong Daero 488beon Gil, Daejeon 34060, South Korea
[3] Korea Aerosp Res Inst, 169-84 Gwahak Ro, Daejeon 34133, South Korea
基金
新加坡国家研究基金会;
关键词
lunar lander; landing stability; classification map; Monte Carlo simulation; landing success rate; HAZARD AVOIDANCE;
D O I
10.3390/aerospace8120380
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper, a method for predicting the landing stability of a lunar lander by a classification map of the landing stability is proposed, considering the soft soil characteristics and the slope angle of the lunar surface. First, the landing stability condition in terms of the safe (=stable), sliding (=unstable), and tip-over (=statically unstable) possibilities was checked by dropping a lunar lander onto flat lunar surfaces through finite-element (FE) simulation according to the slope angle, friction coefficient, and soft/rigid ground, while the vertical touchdown velocity was maintained at 3 m/s. All of the simulation results were classified by a classification map with the aid of logistic regression, a machine-learning classification algorithm. Finally, the landing stability status was efficiently predicted by Monte Carlo (MC) simulation by just referring to the classification map for 10,000 input datasets, consisting of the friction coefficient, slope angles, and rigid/soft ground. To demonstrate the performance, two virtual lunar surfaces were employed based on a 3D terrain map of the LRO mission. Then, the landing stability was validated through landing simulation of an FE model of a lunar lander requiring high computation cost. The prediction results showed excellent agreement with those of landing simulations with a negligible computational cost of around a few seconds.
引用
收藏
页数:16
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  • [1] Touchdown stability simulation of landing gear system for lunar lander
    Beijing Institute of Spacecraft System Engineering, Beijing 100094, China
    [J]. Yuhang Xuebao, 2009, 5 (1792-1796):
  • [2] Soft landing stability of lander in mode of shutdown at touchdown
    Dong, Yang
    Wang, Chunjie
    Wu, Hongyu
    Ding, Zongmao
    Man, Jianfeng
    [J]. Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2019, 45 (02): : 317 - 324
  • [3] Evaluation of Landing Stability of Lunar Lander Considering Various Landing Conditions
    Jeong, Hyun-Jae
    Lim, Jae Hyuk
    Kim, Jin-Won
    [J]. JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2018, 46 (02) : 124 - 132
  • [4] Simulation of Magnetorheological Shock Strut for Lunar Lander Soft Landing
    Wang, Anliu
    Nie, Hong
    Zhang, Ying
    [J]. PROCEEDINGS OF THE SECOND INTERNATIONAL CONFERENCE ON MODELLING AND SIMULATION (ICMS2009), VOL 7, 2009, : 520 - 524
  • [5] Design, Analysis and Stability testing of Lunar Lander for Soft-Landing
    Aravind, G.
    Vishnu, S.
    Amarnath, K., V
    Hithesh, U.
    Harikrishnan, P.
    Sreedharan, Pramod
    Udupa, Ganesh
    [J]. MATERIALS TODAY-PROCEEDINGS, 2020, 24 : 1235 - 1243
  • [6] Analysis on soft-landing dynamics and influence factors of lunar lander
    Dong, Wei-Li
    Liu, Li
    Zhou, Si-Da
    Chen, Shu-Lin
    Zhang, Nan-Fu
    [J]. Yuhang Xuebao/Journal of Astronautics, 2014, 35 (04): : 388 - 396
  • [7] Interval Uncertainty Analysis of Soft-landing Dynamics of Lunar Lander
    Chen, Zhaoyue
    Liu, Li
    Chen, Shulin
    Cui, Ying
    [J]. Binggong Xuebao/Acta Armamentarii, 2019, 40 (02): : 442 - 448
  • [8] Investigation on soft-landing dynamics of four-legged lunar lander
    Wei, Xiaohui
    Lin, Qing
    Nie, Hong
    Zhang, Ming
    Ren, Jie
    [J]. ACTA ASTRONAUTICA, 2014, 101 : 55 - 66
  • [9] Model reduction analysis of soft landing dynamics for lunar lander with local nonlinearities
    Dong, Weili
    Liu, Li
    Zhou, Sida
    [J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2014, 35 (05): : 1319 - 1328
  • [10] Landing stability analysis of the lunar lander based on Monte Carlo approach
    [J]. Song, S. (songshunguang@me.buaa.edu.cn), 1600, Beijing University of Aeronautics and Astronautics (BUAA) (39):