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基于Terminal滑模的小行星探测器着陆连续控制

刘克平 曾建鹏 赵博 李元春

刘克平, 曾建鹏, 赵博, 等 . 基于Terminal滑模的小行星探测器着陆连续控制[J]. 北京航空航天大学学报, 2014, 40(10): 1323-1328. doi: 10.13700/j.bh.1001-5965.2013.0638
引用本文: 刘克平, 曾建鹏, 赵博, 等 . 基于Terminal滑模的小行星探测器着陆连续控制[J]. 北京航空航天大学学报, 2014, 40(10): 1323-1328. doi: 10.13700/j.bh.1001-5965.2013.0638
Liu Keping, Zeng Jianpeng, Zhao Bo, et al. Continuous control for probe landing based on Terminal sliding mode[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(10): 1323-1328. doi: 10.13700/j.bh.1001-5965.2013.0638(in Chinese)
Citation: Liu Keping, Zeng Jianpeng, Zhao Bo, et al. Continuous control for probe landing based on Terminal sliding mode[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(10): 1323-1328. doi: 10.13700/j.bh.1001-5965.2013.0638(in Chinese)

基于Terminal滑模的小行星探测器着陆连续控制

doi: 10.13700/j.bh.1001-5965.2013.0638
基金项目: 国家973重点基础研究发展计划资助项目(2012CB720000)
详细信息
    作者简介:

    刘克平(1971-),男,吉林长春人,教授,liukeping@mail.ccut.edu.cn.

  • 中图分类号: V448.22

Continuous control for probe landing based on Terminal sliding mode

  • 摘要: 针对弱引力场不规则小行星探测器安全下降与着陆,提出了一种基于比例微分(PD,Proportional plus Derivative)及非奇异Terminal滑模的连续控制方法.在着陆点坐标系下推导了探测器的动力学方程,设计了开环燃料次最优多项式标称轨迹制导方法.针对下降和着陆两个不同阶段提出了PD和非奇异Terminal滑模变结构连续控制方法.将PD控制的易操作性与非奇异Terminal滑模控制收敛速度快、调整时间短有效结合,保证了探测器安全着陆.仿真结果表明了提出方法的可行性和有效性.

     

  • [1] Sears D W G, Allen C C,Bell M S,et al.The hera near-earth asteroid sample return mission: science requirements of the sample collector[J].Advances in Space Research,2004,34(11): 22762280
    [2] 崔祜涛, 崔平远.软着陆小行星的自主导航与制导[J].宇航学报,2002,23(5):1-5 Cui Hutao,Cui Pingyuan.Autonomous navigation and guidance for soft-landing asteroid[J].Journal of Astronautics,2002, 23(5): 1-5(in Chinese)
    [3] Li S,Cui P Y, Cui H T.Autonomous navigation and guidance for landing on asteroids[J].Aerospace Science and Technology,2006,10(3):239-247
    [4] Broschart S B, Scheeres D J.Spacecraft descent and translation in the small-body fixed frame[R].AIAA-2004-4865,2004
    [5] Zhang Z X, Wang W D,Li L T,et al.Robust sliding mode guidance and control for soft landing on small bodies[J].Journal of the Franklin Institute,2012,349(2):493-509
    [6] Shao W, Cui P Y,Cui H T.Physical properties calculation of small body using points triangulations[J].Journal of Harbin Institute of Technology,2010,42(5):687-691
    [7] 宋顺广,王春洁. 基于蒙特卡罗法的月球探测器着陆稳定性分析[J].北京航空航天大学学报,2013,39 (9):1192-1196 Song Shunguang,Wang Chunjie.Landing stability analysis of the lunar lander based on Monte Carlo approach[J].Journal of Beijing University of Aeronautics and Astronautics,2013,39(9):1192-1196(in Chinese)
    [8] 高艾,崔平远, 崔祜涛.深空着陆器对偶控制策略[J].哈尔滨工业大学学报,2012,26(11):75-80 Gao Ai,Cui Pingyuan,Cui Hutao.Dual control strategy of planetary lander[J].Journal of Harbin Institute of Technology,2012,26(11):75-80(in Chinese)
    [9] Lan Q X, Li S,Yang J,et al.Finite-time control for soft landing on an asteroid based on line-of-sight angle[J].Journal of the Franklin Institute,2014,351(1):383-398
    [10] 邢健,齐瑞云. 考虑燃料晃动效应的航天器自适应滑模姿态控制[J].空间控制技术与应用,2013,39(2):42-47 Xing Jian,Qi Ruiyun.Adaptive sliding-mode attitude control of spacecraft with fuel sloshing[J].Aerospace Control and Application,2013,39(2):42-47(in Chinese)
    [11] 曾宪法, 王小虎,张晶,等.高超声速飞行器的干扰补偿 Terminal 滑模控制[J].北京航空航天大学学报,2012, 38(11): 1454-1458 Zeng Xianfa,Wang Xiaohu,Zhang Jing,et al.Disturbance compensated terminal sliding mode control for hypersonic vehicles[J].Journal of Beijing University of Aeronautics and Astronautics,2012,38(11):1454-1458(in Chinese)
    [12] Washabaugh P D, Scheeres D J.Energy and stress distributions in ellipsoids[J].Icarus,2002,159(2):314-321
    [13] 单永正. 月球探测器软着陆的制导问题研究[D].哈尔滨:哈尔滨工业大学,2009 Shan Yongzheng.Research on guidance problem of lunar probe for soft landing[D].Harbin:Harbin Institute of Technology,2009(in Chinese)
    [14] 郗晓宁,曾国强, 任萱,等.月球探测器轨道设计[M].北京:国防工业出版社,2001:119-139 Xi Xiaoning,Zeng Guoqiang,Ren Xuan,et al.Lunar probe track design[M].Beijing:National Defense University Press,2001:119-139(in Chinese)
    [15] 孙军伟,崔平远. 月球软着陆多项式制导控制方法[J].宇航学报,2007,28(5):1171-1174 Sun Junwei,Cui Pingyuan.Polynomial guidance law for lunar soft landing[J].Journal of Astronautics,2007,28(5):1171-1174(in Chinese)
    [16] Feng Y, Yu X H,Man Z H.Non-singular terminal sliding mode control of rigid manipulators[J].Automatica,2002,38(12):2159-2167
    [17] 张巍巍, 王京.基于指数趋近律的非奇异Terminal滑模控制[J].控制与决策,2012,27(6):909-913 Zhang Weiwei,Wang Jing.Nonsingular terminal sliding model control based on exponential reaching law[J].Control and Decision,2012,27(6):909-913(in Chinese)

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出版历程
  • 收稿日期:  2013-11-06
  • 网络出版日期:  2014-10-20

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