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空间充气展开绳网系统捕获目标自抗扰控制研究

刘昊 魏承 谭春林 刘永健 赵阳

刘昊, 魏承, 谭春林, 刘永健, 赵阳. 空间充气展开绳网系统捕获目标自抗扰控制研究. 自动化学报, 2019, 45(9): 1691-1700. doi: 10.16383/j.aas.c180835
引用本文: 刘昊, 魏承, 谭春林, 刘永健, 赵阳. 空间充气展开绳网系统捕获目标自抗扰控制研究. 自动化学报, 2019, 45(9): 1691-1700. doi: 10.16383/j.aas.c180835
LIU Hao, WEI Cheng, TAN Chun-Lin, LIU Yong-Jian, ZHAO Yang. Research on Capturing Target of Space Inflatable Net Capture System Based on Active Disturbance Rejection Control. ACTA AUTOMATICA SINICA, 2019, 45(9): 1691-1700. doi: 10.16383/j.aas.c180835
Citation: LIU Hao, WEI Cheng, TAN Chun-Lin, LIU Yong-Jian, ZHAO Yang. Research on Capturing Target of Space Inflatable Net Capture System Based on Active Disturbance Rejection Control. ACTA AUTOMATICA SINICA, 2019, 45(9): 1691-1700. doi: 10.16383/j.aas.c180835

空间充气展开绳网系统捕获目标自抗扰控制研究

doi: 10.16383/j.aas.c180835
基金项目: 

微小型航天器技术国防重点学科实验室开放基金 HIT.KLOF.MST.201703

空间智能控制技术重点实验室开放基金 ZDSYS-2017-07

详细信息
    作者简介:

    刘昊  哈尔滨工业大学航天学院博士研究生.主要研究方向为航天机构动力学控制与仿真.E-mail:liuhaoyt@stu.hit.edu.cn

    谭春林  北京空间飞行器总体设计部研究员.主要研究方向为航天器总体设计.E-mail:tanchunlin1967@sina.com

    刘永健  博士.北京空间飞行器总体设计部研究员.主要研究方向为航天器系统研发.E-mail:liuyj03@126.com

    赵阳  博士.哈尔滨工业大学航天学院教授.主要研究方向为航天器多体动力学与控制, 航天器系统仿真技术.E-mail:yangzhao@hit.edu.cn

    通讯作者:

    魏承  博士.哈尔滨工业大学航天学院副教授.主要研究方向为空间柔性多体系统动力学, 控制与系统仿真技术.本文通信作者. E-mail:weicheng@hit.edu.cn

Research on Capturing Target of Space Inflatable Net Capture System Based on Active Disturbance Rejection Control

Funds: 

Open Fund of National Defense Key Discipline Laboratory of Micro-Spacecraft Technology HIT.KLOF.MST.201703

Open Fund of Science and Technology on Space Intelligent Control Laboratory ZDSYS-2017-07

More Information
    Author Bio:

     Ph. D. candidate at the School of Astronautics, Harbin Institute of Technology. His research interest covers dynamics control and simulation of space mechanism

     Professor at Beijing Institute of Spacecraft System Engineering. His main research interest is spacecraft overall design

     Ph. D., professor at Beijing Institute of Spacecraft System Engineering. His main research interest is spacecraft system development

     Ph. D., professor at the School of Astronautics, Harbin Institute of Technology. His research interest covers spacecraft multi-body dynamics and control, spacecraft system simulation technology

    Corresponding author: WEI Cheng  Ph. D., associate professor at the School of Astronautics, Harbin Institute of Technology. His research interest covers dynamics, control and system simulation technology of space flexible multibody system. Corresponding author of this paper
  • 摘要: 空间充气展开绳网系统是依靠充气梁展开绳网进行目标捕获的航天器系统,具有更好的稳定性和可操控性.然而由于充气梁和绳网的大柔性变形以及捕获失稳自旋目标后的未知碰撞,使得捕获后的航天器姿态稳定控制困难.本文主要基于自抗扰控制解决了空间充气展开绳网系统捕获目标后的姿态稳定和消旋难题.首先,基于理想薄膜充压失效理论和绝对节点坐标方法建立充气展开绳网系统动力学模型,而后设计了航天器姿态稳定自抗扰控制器,用于实时估计并补偿系统捕获过程中未知惯量目标与捕获机构的碰撞干扰.仿真结果表明,动力学模型能够模拟捕获过程中充气梁的屈曲失效及碰撞特性,自抗扰控制器能够有效抑制碰撞带来的干扰,实现空间充气展开绳网系统捕获后的高精度姿态稳定控制,同时能够在有限时间内对自旋目标实现消旋.
    1)  本文责任编委 许斌
  • 图  1  空间充气展开绳网系统任务流程

    Fig.  1  The workflow of SINCS

    图  2  参考坐标系

    Fig.  2  Reference frames

    图  3  简化充气梁

    Fig.  3  Equivalent inflatable boom

    图  4  等效刚度-弯矩

    Fig.  4  Equivalent stiffness-moment

    图  5  尺寸与包络

    Fig.  5  Size and envelope

    图  6  捕获过程

    Fig.  6  Capture process

    图  7  等效刚度变化

    Fig.  7  Change of equivalent stiffness

    图  8  目标碰撞力

    Fig.  8  Collision of target

    图  9  服务航天器位移

    Fig.  9  Displacement of spacecraft

    图  10  控制器框图

    Fig.  10  Controller structure

    图  11  姿态稳定和消旋过程

    Fig.  11  Attitude stabilization and despinning

    图  12  服务航天器姿态对比曲线

    Fig.  12  Attitude curve of spacecraft

    图  13  干扰估计

    Fig.  13  Estimation of disturbance

    图  14  控制力矩

    Fig.  14  Torque of controller

    图  15  目标碰撞力

    Fig.  15  Collision of target

    图  16  目标角速度

    Fig.  16  Angular velocity of target

    表  1  服务航天器和捕获目标参数

    Table  1  Parameters of spacecraft and target

    Name Value
    Rotational inertia of spacecraft
    (kg·m2)
    diag{900, 800, 1 000}
    Size of spacecraft (m) 2.5×2.5×4
    Size of capture mechanism (m) ${l_d} = 0.4, {l_u} = 4, h = 4$
    Rotational inertia of target ($\rm {kg\cdot{m^2}}$) diag{500, 500, 700}
    Size of target (m) 1.3×1.3×1.0
    下载: 导出CSV

    表  2  绳网和充气梁参数

    Table  2  Parameters of net and inflatable boom

    Name Nets Inflatable booms
    Diameter (m) 0.006 0.1
    Density ($\rm {kg/{m^2}}$) 1 430 64
    Poisson ratio 0.3 0.3
    Modulus of elasticity (GPa) 12 ${E_1}=0.15, {E_2}=0.075$
    Bending moment ($\rm {N\cdot{m}}$) - ${M_1}=5, {M_2}=10$
    下载: 导出CSV
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出版历程
  • 收稿日期:  2018-12-17
  • 录用日期:  2019-04-23
  • 刊出日期:  2019-09-20

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