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基于backstepping/RHO的变体飞机控制器设计

陈伟 卢京潮 王晓光 章卫国

陈伟, 卢京潮, 王晓光, 等 . 基于backstepping/RHO的变体飞机控制器设计[J]. 北京航空航天大学学报, 2014, 40(8): 1060-1065. doi: 10.13700/j.bh.1001-5965.2013.0510
引用本文: 陈伟, 卢京潮, 王晓光, 等 . 基于backstepping/RHO的变体飞机控制器设计[J]. 北京航空航天大学学报, 2014, 40(8): 1060-1065. doi: 10.13700/j.bh.1001-5965.2013.0510
Chen Wei, Lu Jingchao, Wang Xiaoguang, et al. Design of a controller for morphing aircraft based on backstepping/RHO[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(8): 1060-1065. doi: 10.13700/j.bh.1001-5965.2013.0510(in Chinese)
Citation: Chen Wei, Lu Jingchao, Wang Xiaoguang, et al. Design of a controller for morphing aircraft based on backstepping/RHO[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(8): 1060-1065. doi: 10.13700/j.bh.1001-5965.2013.0510(in Chinese)

基于backstepping/RHO的变体飞机控制器设计

doi: 10.13700/j.bh.1001-5965.2013.0510
基金项目: 

国家自然科学基金资助项目(60974146);航空科学基金资助项目(20100753009)

详细信息
    作者简介:

    陈伟(1986-),男,湖北随州人,博士生,chenwei1298@mail.nwpu.edu.cn.

  • 中图分类号: V249.1

Design of a controller for morphing aircraft based on backstepping/RHO

  • 摘要: 为了确保变体飞机在变体过程中的飞行稳定性,提出了一种并行修正控制器设计方案.采用backstepping方法进行标称控制器设计,提供基本的飞行稳定性和跟踪性能.使用雅可比线性化方法对变体飞机非线性方程进行线性化得到线性化模型,采用基于指令滤波器的滚动时域优化(RHO,Receding Horizon Optimal)方法进行修正控制器设计.在有限时域区间内实时解算修正控制量,对标称控制器进行补偿.从航迹角控制系统仿真结果可以看出,航迹角能够较好地跟踪指令信号,基本不受变体过程的影响,飞行控制系统满足实时性和鲁棒性的要求.

     

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出版历程
  • 收稿日期:  2013-09-22
  • 刊出日期:  2014-08-20

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