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具有预定指数收敛特性的线性系统最小能量输出反馈控制

董乘麟,  赵凯,  叶合夫,  宋永端

董乘麟, 赵凯, 叶合夫, 宋永端. 具有预定指数收敛特性的线性系统最小能量输出反馈控制. 自动化学报, xxxx, xx(x): x−xx doi: 10.16383/j.aas.c260114
引用本文: 董乘麟, 赵凯, 叶合夫, 宋永端. 具有预定指数收敛特性的线性系统最小能量输出反馈控制. 自动化学报, xxxx, xx(x): x−xx doi: 10.16383/j.aas.c260114
Dong Cheng-Lin, Zhao Kai, Ye He-Fu, Song Yong-Duan. Minimum-energy output feedback control of linear systems with predefined exponential convergence. Acta Automatica Sinica, xxxx, xx(x): x−xx doi: 10.16383/j.aas.c260114
Citation: Dong Cheng-Lin, Zhao Kai, Ye He-Fu, Song Yong-Duan. Minimum-energy output feedback control of linear systems with predefined exponential convergence. Acta Automatica Sinica, xxxx, xx(x): x−xx doi: 10.16383/j.aas.c260114

具有预定指数收敛特性的线性系统最小能量输出反馈控制

doi: 10.16383/j.aas.c260114 cstr: 32138.14.j.aas.c260114
基金项目: 国家自然科学基金(62403082, W2411061), 重庆市自然科学基金(CSTB2023NSCQ-LZX0026)资助
详细信息
    作者简介:

    董乘麟:重庆大学自动化学院硕士研究生. 2025年获得重庆大学机器人工程专业学士学位. 主要研究方向为最优控制与预设时间控制. E-mail: dongchenglin@stu.cqu.edu.cn

    赵凯:重庆大学自动化学院教授. 2019年获重庆大学控制理论与控制工程专业博士学位. 主要研究方向为预设性能控制, 自适应控制, 约束控制, 智能控制系统和机器人控制及其应用. 本文通信作者. E-mail: zhaokai@cqu.edu.cn

    叶合夫:重庆大学博士. 2025年获得重庆大学控制科学与工程专业博士学位. 主要研究方向为预设时间控制. E-mail: hefuye@cuhk.edu.hk

    宋永端:中国工程院外籍院士, 重庆大学自动化学院教授. 主要研究方向为智能控制, 容错控制, 自适应协调控制, 飞行器导航与控制, 复杂系统主动安全预警与控制. E-mail: ydsong@cqu.edu.cn

Minimum-energy Output Feedback Control of Linear Systems With Predefined Exponential Convergence

Funds: Supported by National Natural Science Foundation of China (62403082, W2411061) and Natural Science Foundation of Chongqing (CSTB2023NSCQ-LZX0026)
More Information
    Author Bio:

    DONG Cheng-Lin Master student at the School of Automation, Chongqing University. He received his bachelor degree in robotics engineering from Chongqing University in 2025. His research interests include optimal control and prescribed-time control

    ZHAO Kai Professor at the School of Automation, Chongqing University. He received his Ph. D. degree in control theory and control engineering from Chongqing University in 2019. His research interest covers prescribed performance control, adaptive control, constrained control, intelligent control systems, and robotic control and applications. Corresponding author of this paper

    YE He-Fu Ph.D. of Chongqing University. He received his Ph. D. degree in control science and engineering from Chongqing University in 2025. His main research interest is prescribed-time control

    SONG Yong-Duan Foreign Academician of Chinese Academy of Engineering, professor at the School of Automation, Chongqing University. His research interests include intelligent control, fault-tolerant control, adaptive cooperative control, aircraft navigation and control, and active safety early-warning and control for complex systems

  • 摘要: 针对线性系统, 研究预定指数收敛速度下的最小能量输出反馈控制问题. 不同于传统的线性二次型调节器方法, 此问题的挑战在于: 1) 保证状态观测器与控制器预定指数收敛速度与能量最小的协同优化; 2)在稳定性分析过程中, 由于观测误差与状态估计之间的耦合项, 导致难以保证Lyapunov函数导数的负定性. 为解决以上难题, 提出一种基于系统变换的预定收敛速度控制与矩阵束解耦优化方法, 其核心与创新在于: 1) 根据系统模型的对偶系统, 将其对应的代数Riccati方程解嵌入观测器设计, 使得系统观测误差具有预定的指数收敛速度并保证能量最小; 2) 在稳定性分析过程中, 针对观测误差与状态估计之间的耦合项, 利用矩阵束理论, 建立Lyapunov函数与耦合项之间的代数关系, 保证其导数的负定性, 进而实现系统的增广状态向量按照预定收敛速度镇定并给出能量最小条件, 降低了算法的保守性. 仿真结果验证了方法的有效性.
  • 图  1  不同$ \gamma $值下系统状态响应曲线

    Fig.  1  Response curves of system states under different values of $ \gamma $

    图  2  不同初始状态下系统状态响应曲线

    Fig.  2  Response curves of system states under different initial values

    图  3  不同极点配置下各性能指标值

    Fig.  3  Performance index values under different pole placements

    图  4  不同初始值下的系统状态估计$ \hat x_1(t) $与观测误差$ e_1(t) $响应曲线

    Fig.  4  Response curves of system state estimate $ \hat x_1(t) $ and observer error $ e_1(t) $ under different initial values

    图  5  不同初始值下的系统状态估计$ \hat x_2(t) $与观测误差$ e_2(t) $响应曲线

    Fig.  5  Response curves of system state estimate $ \hat x_2(t) $ and observer error $ e_2(t) $ under different initial values

    图  6  不同初始值下的性能指标值

    Fig.  6  Performance index values under different initial values

    图  7  LQR方法与所提方法下的系统状态估计$ \hat x_1(t) $与观测误差$ e_1(t) $响应曲线

    Fig.  7  Response curves of system state estimate $ \hat x_1(t) $ and observer error $ e_1(t) $ under the LQR method and the proposed method

    图  8  LQR方法与所提方法下的系统状态估计$ \hat x_2(t) $与观测误差$ e_2(t) $响应曲线

    Fig.  8  Response curves of system state estimate $ \hat x_2(t) $ and observer error $ e_2(t) $ under the LQR method and the proposed method

    图  9  文献[37]方法与所提方法状态估计响应曲线

    Fig.  9  State estimation response curves of the method in reference [37] and the proposed method

    图  12  文献[37]方法与所提方法性能指标$ J $变化曲线

    Fig.  12  Performance index $ J $ variation curves of the method in reference [37] and the proposed method

    图  11  文献[37]方法与所提方法控制输入响应曲线

    Fig.  11  Control input response curves of the method in reference [37] and the proposed method

    图  10  文献[37]方法与所提方法状态估计误差范数响应曲线

    Fig.  10  State estimation error norm response curves of the method in reference [37] and the proposed method

    图  13  VTOL模型示意图

    Fig.  13  Schematic diagram of the VTOL model

    图  14  VTOL系统状态$ x(t) $与状态估计$ \hat{x}(t) $响应曲线

    Fig.  14  Response curves of state $ x(t) $ and its state estimate $ \hat x(t) $ of VTOL system

    图  15  VTOL系统状态控制输入响应曲线

    Fig.  15  Response curves of system states and control inputs of VTOL system

    表  1  仿真极点配置

    Table  1  Pole placements for simulation

    最优 Pole$ _1 $ Pole$ _2 $ Pole$ _3 $ Pole$ _4 $
    $ \begin{bmatrix} -1.158 1\\-1.241 8 \end{bmatrix} $ $ \begin{bmatrix} -0.705 5\\-0.900 0 \end{bmatrix} $ $ \begin{bmatrix} -3.000 0\\-2.500 0 \end{bmatrix} $ $ \begin{bmatrix} -0.577 8\\-0.650 0 \end{bmatrix} $ $ \begin{bmatrix} -5.000 0\\-5.800 0 \end{bmatrix} $
    下载: 导出CSV

    表  2  系统状态初始值

    Table  2  Initial value of system states

    Case 1 Case 2 Case 3
    $ x(0) $=[1.2, 1.5]$ ^{\text{T}} $ $ x(0) $=[1.2, 1.5]$ ^{\text{T}} $ $ x(0) $=[1.2, 1.5]$ ^{\text{T}} $
    $ \hat{x}(0) $=[1.2, 1.5]$ ^{\text{T}} $ $ \hat{x}(0) $=[0.0, 0.0]$ ^{\text{T}} $ $ \hat{x}(0) $=[2.0, 2.3]$ ^{\text{T}} $
    下载: 导出CSV
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  • 收稿日期:  2026-02-07
  • 录用日期:  2026-05-27
  • 网络出版日期:  2026-10-22

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