留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

基于响应面法的月球着陆器软着陆性能优化

王家俊 王春洁 宋顺广

王家俊, 王春洁, 宋顺广等 . 基于响应面法的月球着陆器软着陆性能优化[J]. 北京航空航天大学学报, 2014, 40(5): 707-711. doi: 10.13700/j.bh.1001-5965.2013.0364
引用本文: 王家俊, 王春洁, 宋顺广等 . 基于响应面法的月球着陆器软着陆性能优化[J]. 北京航空航天大学学报, 2014, 40(5): 707-711. doi: 10.13700/j.bh.1001-5965.2013.0364
Wang Jiajun, Wang Chunjie, Song Shunguanget al. Performance optimization of lunar lander based on response surface methodology[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(5): 707-711. doi: 10.13700/j.bh.1001-5965.2013.0364(in Chinese)
Citation: Wang Jiajun, Wang Chunjie, Song Shunguanget al. Performance optimization of lunar lander based on response surface methodology[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(5): 707-711. doi: 10.13700/j.bh.1001-5965.2013.0364(in Chinese)

基于响应面法的月球着陆器软着陆性能优化

doi: 10.13700/j.bh.1001-5965.2013.0364
详细信息
    作者简介:

    王家俊(1990- ),男,河北定州人,硕士生,wangjiajun@me.buaa.edu.cn.

  • 中图分类号: V11

Performance optimization of lunar lander based on response surface methodology

  • 摘要: 为了提高月球着陆器软着陆性能,建立了月球着陆器的多体动力学参数化模型.对某典型恶劣工况进行了优化拉丁超立方实验设计,辨识关键实验因子.利用参数化模型和实验设计获取样本点构造了响应面模型,并检验了响应面的拟合精度.以多个动力学性能作为优化目标,用响应面计算结果构造目标函数和约束条件,对响应面参数做多目标优化.将优化所得参数代入动力学模型中进行仿真,优化效果明显,验证了基于响应面法的软着陆性能优化方法的可行性,为今后的仿真实验提供参考.

     

  • [1] 曾福明, 杨建中,满剑锋,等.月球着陆器着陆缓冲机构设计方法研究[J].航天器工程,2011,20(2):46-51 Zeng Fuming,Yang Jianzhong,Man Jianfeng,et al.Study of design method of landing gear for lunar lander[J].Spacecraft Engineering,2011,20(2):46-51(in Chinese)
    [2] 逯运通, 宋顺广,王春洁,等.基于刚柔耦合模型的月球着陆器动力学分析[J].北京航空航天大学学报,2010,36(11):1348-1352 Lu Yuntong,Song Shunguang,Wang Chunjie,et al.Dynamic analysis for lunar lander based on rigid-flexible coupled model[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(11):1348-1352(in Chinese)
    [3] Hilderman R A, Mueller W H,Mantus M.Landing dynamics of the lunar excursion module[J].Journal of Spacecraft and Rockets,1966,3(10):1484-1489
    [4] 朱汪,杨建中. 月球探测器软着陆机构着陆腿模型与仿真分析[J].宇航学报,2008,29(6):1723-1728 Zhu Wang,Yang Jianzhong.Modeling and simulation of landing leg for the lunar landing gear system[J].Journal of Astronautics,2008,29(6):1723-1728(in Chinese)
    [5] Lavender R E. A Monte Carlo approach to touchdown dynamics for soft lunar landings[R].NASA-TN-D-3117,1965
    [6] Lu Y T, Wang C J,Zeng F M,et al.A Monte Carlo analysis of lunar lander dynamics at touchdown[C]//CSAA.Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology.Xi'an:Northwestern Polytechnical University Press,2010:481-484
    [7] Marler R T, Arora J S.Survey of multi-objective optimization methods for engineering[J].Structural and Multidisciplinary Optimization,2004,26(6):369-395
    [8] 刘晓路,陈英武, 荊显荣,等.优化拉丁方试验设计方法及其应用[J].国防科技大学学报,2011,33(5):73-77 Liu Xiaolu,Chen Yingwu,Jing Xianrong,et al.Optimized latin hypercube sampling method and its application[J].Journal of National University of Defence Technology,2011,33(5):73-77(in Chinese)
    [9] Khuri A I, Mukhopadhyay S.Response surface methodology[J].WIREs Computational Statistics,2010,2(2):128-149
    [10] 方开泰,全辉, 陈庆云.实用回归分析[M].北京:科学出版社,1988:29-35,151-152 Fang Kaitai,Quan Hui,Chen Qingyun.Practical regression analysis[M].Beijing:Science Press,1988:29-35,151-152(in Chinese)
    [11] Srinivas N, Deb K.Multiobjective optimization using nondominated sorting in genetic algorithms[J].Evolutionary Computation,1994,2(3):221-248
    [12] Deb K, Pratap A,Agarwal S,et al.A fast and elitist multiobjective genetic algorithm:NSGA-II[J].IEEE Transactions on Evolutionary Computation,2002,6(2):182-197
  • 加载中
计量
  • 文章访问数:  1071
  • HTML全文浏览量:  18
  • PDF下载量:  560
  • 被引次数: 0
出版历程
  • 收稿日期:  2013-06-25
  • 刊出日期:  2014-05-20

目录

    /

    返回文章
    返回
    常见问答