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基于模糊滑模控制的CAV再入标准轨迹制导

黄康强 赵辉 任洋 蔡亚伟

黄康强, 赵辉, 任洋, 等 . 基于模糊滑模控制的CAV再入标准轨迹制导[J]. 北京航空航天大学学报, 2015, 41(9): 1749-1757. doi: 10.13700/j.bh.1001-5965.2014.0742
引用本文: 黄康强, 赵辉, 任洋, 等 . 基于模糊滑模控制的CAV再入标准轨迹制导[J]. 北京航空航天大学学报, 2015, 41(9): 1749-1757. doi: 10.13700/j.bh.1001-5965.2014.0742
HUANG Kangqiang, ZHAO Hui, REN Yang, et al. Standard trajectory guidance for CAV reentry based on fuzzy sliding mode control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(9): 1749-1757. doi: 10.13700/j.bh.1001-5965.2014.0742(in Chinese)
Citation: HUANG Kangqiang, ZHAO Hui, REN Yang, et al. Standard trajectory guidance for CAV reentry based on fuzzy sliding mode control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(9): 1749-1757. doi: 10.13700/j.bh.1001-5965.2014.0742(in Chinese)

基于模糊滑模控制的CAV再入标准轨迹制导

doi: 10.13700/j.bh.1001-5965.2014.0742
基金项目: 国家自然科学基金青年科学基金(61203628)
详细信息
    作者简介:

    黄康强(1991—),男,湖南益阳人,硕士研究生,huangkangqianglh@163.com

    通讯作者:

    赵辉(1973—),男,河北任丘人,教授,kgy_zhao@163.com,主要研究方向为无人飞行器作战系统与技术.

  • 中图分类号: V448.23

Standard trajectory guidance for CAV reentry based on fuzzy sliding mode control

  • 摘要: 针对标准轨迹制导对状态初值过于敏感以及鲁棒性较差的问题,在模糊滑模控制的基础上,提出了一种新的标准轨迹制导方式.通过滑模控制的鲁棒性来提升制导方法的适应能力,利用模糊系统的万能逼近特性来对不确定因素进行逼近,从而实现对不确定项的准确估计.对隶属度函数的建立原则进行了分析, 结合再入特点建立了模糊滑模纵向制导方案,仿真结果验证了模糊逼近与状态反馈总控制律的有效性,在此基础上设计了侧向制导律.仿真结果表明:该方法能够在保证精度的同时提高标准轨迹制导的鲁棒性,使计算过程大大简化.

     

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出版历程
  • 收稿日期:  2014-11-28
  • 刊出日期:  2015-09-20

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