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基于DM-DSC的舰载机着舰自动复飞控制算法

崔凯凯 韩维 刘玉杰 刘洁 褚达文 崔荣伟

崔凯凯,韩维,刘玉杰,等. 基于DM-DSC的舰载机着舰自动复飞控制算法[J]. 北京航空航天大学学报,2023,49(4):900-912 doi: 10.13700/j.bh.1001-5965.2021.0362
引用本文: 崔凯凯,韩维,刘玉杰,等. 基于DM-DSC的舰载机着舰自动复飞控制算法[J]. 北京航空航天大学学报,2023,49(4):900-912 doi: 10.13700/j.bh.1001-5965.2021.0362
CUI K K,HAN W,LIU Y J,et al. Automatic wave-off control algorithm for carrier aircraft based on DM-DSC[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(4):900-912 (in Chinese) doi: 10.13700/j.bh.1001-5965.2021.0362
Citation: CUI K K,HAN W,LIU Y J,et al. Automatic wave-off control algorithm for carrier aircraft based on DM-DSC[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(4):900-912 (in Chinese) doi: 10.13700/j.bh.1001-5965.2021.0362

基于DM-DSC的舰载机着舰自动复飞控制算法

doi: 10.13700/j.bh.1001-5965.2021.0362
基金项目: 国家自然科学基金(62003366)
详细信息
    通讯作者:

    E-mail:liuyexiaobao@163.com

  • 中图分类号: V249.12

Automatic wave-off control algorithm for carrier aircraft based on DM-DSC

Funds: National Natural Science Foundation of China (62003366)
More Information
  • 摘要:

    针对理想复飞轨迹已知条件下的舰载机自动复飞控制问题,提出一种基于偏差模型的动态面控制(DM-DSC)算法。基于Radau伪谱法给出了舰载机着舰的最优复飞轨迹;根据得到的最优复飞轨迹及其所对应的控制方案,分别给出了速度子系统和高度子系统的偏差控制模型和反演(Backstepping)控制器,并通过引入动态面结构来获得虚拟控制量的微分信号,避免了Backstepping控制律求解过程中的“微分膨胀”问题;考虑到气动参数的不确定性及舰尾流场的干扰,采用线性扩张状态观测器(LESO)对控制模型中的干扰项进行估计和补偿,并设计抗饱和辅助系统来抑制控制饱和的不利影响;最后,基于Lyapunov方法证明闭环系统信号的有界性。仿真结果表明:所提算法具有良好的控制性能。

     

  • 图 1  舰载机着舰复飞示意图

    Figure 1.  Wave-off diagram of carrier aircraft

    图 2  自动复飞控制系统结构示意图

    Figure 2.  Diagram of automatic wave-off control system

    图 3  水平和垂直方向舰尾流强度

    Figure 3.  Horizontal and vertical intensity of carrier air wake

    图 4  速度子系统跟踪控制误差

    Figure 4.  Tracking control errors of speed subsystem

    图 5  高度子系统跟踪控制结果

    Figure 5.  Tracking control results of altitude subsystem

    图 6  高度子系统跟踪控制误差

    Figure 6.  Tracking control errors of altitude subsystem

    图 7  控制系统油门输入

    Figure 7.  Throttle input of control system

    图 8  发动机油门输出响应

    Figure 8.  Output response of engine thrust

    图 9  控制系统舵偏角输入

    Figure 9.  Elevator deflection input of control system

    图 10  舵偏角输入变化率

    Figure 10.  Rate of change of elevator deflection input

    图 11  抗饱和系统的补偿信号

    Figure 11.  Compensation signal of anti-saturation system

    图 12  未知干扰的估计结果

    Figure 12.  Estimation results of unknown disturbances

    图 13  LESO的估计误差

    Figure 13.  Estimation errors of LESO

    图 14  速度子系统跟踪控制结果

    Figure 14.  Tracking control results of speed subsystem

    表  1  舰载机状态/控制变量的容许范围

    Table  1.   Admissible ranges of state and control variables

    状态/控制变量$\alpha $/(°) $q$ ${\delta _{{P} } }$$ {\delta _{\text{e}}} $/(°)$ {\dot \delta _{\text{e}}} $/((°)·s−1)
    容许取值范围[1, 20][−1, 1][0, 1][−24, 10.5][−40, 40]
    下载: 导出CSV
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出版历程
  • 收稿日期:  2021-06-30
  • 录用日期:  2021-09-30
  • 网络出版日期:  2021-11-02
  • 整期出版日期:  2023-04-30

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