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基于改进ESO的星间激光通信精跟踪自适应自抗扰控制

李伟鹏 刘泽书 包泽宇 乔建忠 朱玉凯

李伟鹏, 刘泽书, 包泽宇, 乔建忠, 朱玉凯. 基于改进ESO的星间激光通信精跟踪自适应自抗扰控制. 自动化学报, 2025, 51(12): 1−15 doi: 10.16383/j.aas.c250102
引用本文: 李伟鹏, 刘泽书, 包泽宇, 乔建忠, 朱玉凯. 基于改进ESO的星间激光通信精跟踪自适应自抗扰控制. 自动化学报, 2025, 51(12): 1−15 doi: 10.16383/j.aas.c250102
Li Wei-Peng, Liu Ze-Shu, Bao Ze-Yu, Qiao Jian-Zhong, Zhu Yu-Kai. Adaptive adrc for the fine tracking system in inter-satellite laser communication based on improved eso. Acta Automatica Sinica, 2025, 51(12): 1−15 doi: 10.16383/j.aas.c250102
Citation: Li Wei-Peng, Liu Ze-Shu, Bao Ze-Yu, Qiao Jian-Zhong, Zhu Yu-Kai. Adaptive adrc for the fine tracking system in inter-satellite laser communication based on improved eso. Acta Automatica Sinica, 2025, 51(12): 1−15 doi: 10.16383/j.aas.c250102

基于改进ESO的星间激光通信精跟踪自适应自抗扰控制

doi: 10.16383/j.aas.c250102 cstr: 32138.14.j.aas.c250102
基金项目: 国家自然科学基金(62473016), 北京市自然科学基金(4232048), 动态光学成像与测量全国重点实验室开放课题(2025001)资助
详细信息
    作者简介:

    李伟鹏:北京航空航天大学宇航学院副研究员. 主要研究方向为空间精密载荷振动隔离/抑制, 精密结构/机构设计及控制. E-mail: liweipeng@buaa.edu.cn

    刘泽书:北京航空航天大学宇航学院博士研究生. 主要研究方向为精密机构设计及控制, 卫星激光通信. E-mail: liuzs1@buaa.edu.cn

    包泽宇:北京航空航天大学宇航学院博士研究生. 主要研究方向为卫星制造, 激光通信. E-mail: baozeyu@buaa.edu.cn

    乔建忠:北京航空航天大学自动化学院教授. 主要研究方向为故障诊断与容错控制, 抗扰动控制和微小卫星姿态控制. E-mail: jzqiaobuaa@126.com

    朱玉凯:北京航空航天大学宇航学院副教授. 主要研究方向为抗扰动控制, 滑模控制和航天器姿态控制. 本文通信作者. E-mail: yukaizhu@buaa.edu.cn

Adaptive ADRC for the Fine Tracking System in Inter-satellite Laser Communication Based on Improved ESO

Funds: Supported by National Natural Science Foundation of China (62473016), Beijing Natural Science Foundation (4232048), and Open Fund of the State Key Laboratory of Dynamic Optical Imaging and Measurement(2025001)
More Information
    Author Bio:

    LI Wei-Peng Associate researcher at the School of Astronautics, Beihang University. His research interests include space precision load vibration isolation/suppression and precision structure/mechanism design and control

    LIU Ze-Shu Ph.D. candidate at the School of Astronautics, Beihang University. His researc interests include precision mechanism design and control and satellite laser communication

    BAO Ze-Yu Ph.D. candidate at the School of Astronautics, Beihang University. His research interests include satellite manufacture and laser communication

    QIAO Jian-Zhong Professor at the School of Automation, Beihang University His research interests include fault diagnosis and tolerant control, anti-disturbance control, and attitude control of microsatellite

    ZHU Yu-Kai Associate professor at the School of Astronautics, Beihang University. His research interests include anti-disturbance control, sliding mode control, and attitude control of spacecrafts. Corresponding author of this paper

  • 摘要: 星间激光通信中的光束指向误差会显著降低链路质量. 精跟踪系统因其高带宽特性, 主要负责对高频扰动进行实时修正. 针对精跟踪环节所面临的高频扰动, 传统自抗扰控制(ADRC)在扰动估计与补偿方面仍存在性能瓶颈. 本文考虑一种特殊的干扰形式, 并基于此构造具备频率分离能力的改进扩张状态观测器(ESO), 实现对快慢变扰动的解耦. 在此基础上提出一种融合自适应滤波的自适应ADRC框架, 该方法在传统ADRC框架基础上, 引入并联自适应滤波器, 通过滤波器权重在线更新实现对光束指向误差的自适应抑制, 提升系统在高频干扰下的控制性能. 实验结果表明, 所提方法相比传统控制方法具有更强的扰动抑制能力.
  • 图  1  动力学模型示意图

    Fig.  1  Schematic diagram of dynamic model

    图  2  频率分离特性

    Fig.  2  Frequency decoupling characteristic

    图  3  调参流程图

    Fig.  3  Parameter tuning flowchart

    图  4  控制框图

    Fig.  4  Control block diagram

    图  5  激光通信捕跟控制算法实验平台

    Fig.  5  Experimental platform for laser communication acquisition and tracking control algorithm

    图  6  低频干扰的观测

    Fig.  6  Observation of low-frequency disturbance

    图  7  高频干扰的观测

    Fig.  7  Observation of high-frequency disturbance

    图  8  复合干扰的观测

    Fig.  8  Observation of composite disturbance

    图  9  复合干扰下慢变干扰的观测

    Fig.  9  Observation of slow-varying disturbance under composite disturbance

    图  11  复合干扰下集总干扰的观测

    Fig.  11  Observation of total disturbance under composite disturbance

    图  10  复合干扰下快变干扰的观测

    Fig.  10  Observation of fast-varying disturbance under composite disturbance

    图  12  本文方法与传统ESO对比((a)估计结果; (b)估计误差)

    Fig.  12  Comparison between the proposed method and traditional ESO ((a) Estimation results; (b) Estimation errors)

    图  13  快变干扰估计与慢变干扰估计的FRF曲线

    Fig.  13  Fast-varying disturbance estimation and slow-varying disturbance estimation FRF curves

    图  14  光束抖动抑制实验的时域响应曲线

    Fig.  14  Time-domain response curves of beam jitter suppression experiment

    图  15  不同方法的控制效果((a) $30 \sim 35$s内的功率谱密度; (b) $55 \sim 60$s内的功率谱密度)

    Fig.  15  Control effects of different methods ((a) Power spectrum density in $30 \sim 35$s; (b) Power spectrum density in $55 \sim 60$s)

    表  1  星上主要扰源及其干扰形式

    Table  1  Main disturbance sources on the satellite and their disturbance forms

    扰源 干扰形式
    反作用飞轮、控制力矩陀螺、动量轮 多频线谱和宽频噪声
    天线等驱动机构 多频线谱和宽频噪声
    三浮陀螺 宽频噪声
    磁力矩器 宽频噪声
    下载: 导出CSV

    表  2  激光通信捕跟控制算法实验平台中快反镜的参数

    Table  2  Parameters of fast steering mirror in experimental platform for laser communication acquisition and tracking control algorithm

    方向 $ a_1 $ (1/s) $ a_2 $ (1/$ {\rm{s}}^2 $) b ($ 10^{-6} {\rm{rad}}/({\rm{s}}^2 \cdot V) $)
    x 1 809 $ 7.301 \times 10^6 $ $ 6.079 \times 10^6 $
    y(真实器件) 1 981 $ 7.487 \times 10^6 $ $ 4.736 \times 10^6 $
    y(控制器设计) 1 809 $ 7.301 \times 10^6 $ $ 6.079 \times 10^6 $
    下载: 导出CSV

    表  3  实验中使用的控制器参数

    Table  3  Parameters of controllers used in experiment

    本文方法 PID 传统LADRC FxLMS+PID
    σ $ 2\times 10^{-6} $ - - -
    $ k_p $ 0.43 0.43 0.95 0.43
    $ k_i $ 1 339 1 339 - 1 339
    $ k_d $ $ 3.5 \times 10 ^{-5} $ $ 3.5 \times 10 ^{-5} $ $ -3.5 \times 10 ^{-5} $ $ 3.5 \times 10 ^{-5} $
    $ \omega_o $ 400 - 400 -
    μ $ \mathrm{1\times 10^{-6}} $ - - $ 5\times 10^{-8}(x) $, $ 3\times 10^{-6}(y) $
    M 128 - - 128
    下载: 导出CSV

    表  4  改进ESO与传统ESO估计性能对比(V)

    Table  4  Comparison of estimation performance between improved and traditional ESO (V)

    最大绝对误差 平均误差 均方根误差
    传统ESO x $ {\bf 0.995} $ $ \bf -0.026 $ $ {\bf 0.487} $
    y $ {\bf 1.119} $ $ -0.041 $ $ {\bf 0.492} $
    改进ESO x $ 1.038 $ $ \bf -0.026 $ $ 0.499 $
    y $ 1.137 $ $ {\bf -0.040} $ $ 0.504 $
    下载: 导出CSV

    表  5  不同控制方法下指向误差的均方根($ 10^{-6} $rad)

    Table  5  RMS of pointing error under different methods ($ 10^{-6} $rad)

    控制方法 x y
    $ 30 \sim 35 $s $ 55 \sim 60 $s $ 30 \sim 35 $s $ 55 \sim 60 $s
    无控制 100.26 101.10 93.15 94.13
    传统LADRC 51.54 52.71 52.52 53.30
    PID 31.45 34.73 25.45 27.03
    FxLMS+PID 32.60 35.54 8.04 8.73
    本文方法 8.08 8.04 5.30 5.35
    下载: 导出CSV
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