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基于非线性模型预测的绳系系统系绳摆振控制

张宇靖 钟睿

张宇靖, 钟睿. 基于非线性模型预测的绳系系统系绳摆振控制[J]. 北京航空航天大学学报, 2018, 44(10): 2200-2207. doi: 10.13700/j.bh.1001-5965.2017.0810
引用本文: 张宇靖, 钟睿. 基于非线性模型预测的绳系系统系绳摆振控制[J]. 北京航空航天大学学报, 2018, 44(10): 2200-2207. doi: 10.13700/j.bh.1001-5965.2017.0810
ZHANG Yujing, ZHONG Rui. Tether swing control of tethered system based on nonlinear model prediction[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(10): 2200-2207. doi: 10.13700/j.bh.1001-5965.2017.0810(in Chinese)
Citation: ZHANG Yujing, ZHONG Rui. Tether swing control of tethered system based on nonlinear model prediction[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(10): 2200-2207. doi: 10.13700/j.bh.1001-5965.2017.0810(in Chinese)

基于非线性模型预测的绳系系统系绳摆振控制

doi: 10.13700/j.bh.1001-5965.2017.0810
基金项目: 

国家自然科学基金 11402009

详细信息
    作者简介:

    张宇靖  男, 硕士研究生。主要研究方向:绳系卫星控制相关方向

    钟睿  男, 博士, 副教授, 硕士生导师。主要研究方向:航天动力学和控制

    通讯作者:

    钟睿, E-mail:zhongruia@163.com

  • 中图分类号: V448.12

Tether swing control of tethered system based on nonlinear model prediction

Funds: 

National Natural Science Foundation of China 11402009

More Information
  • 摘要:

    针对绳系系统离轨稳定控制问题,开展了系绳和绳端卫星构成的绳系系统在拖拽离轨过程中系绳摆动稳定控制方法研究。在考虑拖拽离轨过程中约束下,首先建立了包含绳端卫星的姿态运动的模型,并建立了绳系系统的离轨动力学方程和便于控制器设计的简化动力学方程。其次根据模型预测原理以最优化方法设计参考轨迹,最后以模型预测控制方法为基础设计了稳定系绳摆动的非线性模型预测控制方法。使用MATLAB软件平台仿真,验证了所设计的参考轨迹能完成目标和模型预测控制器有好的跟踪能力。

     

  • 图 1  绳系系统坐标系示意图

    Figure 1.  Schematic of coordinate system of tethered system

    图 2  系绳面内摆角、系绳面内摆角速度、主星俯仰角、主星俯仰角速度和绳速的实际路径和最优路径

    Figure 2.  Actual path and optimal path of tether's in-plane swing angle, tether's in-plane swing angular velocity, main satellite pitching angle, main satellite pitching angular velocity and tether speed

    图 3  系绳面内摆角、系绳面内摆角速度、主星俯仰角、主星俯仰角速度和绳速的跟踪路径和最优路径

    Figure 3.  Tracking path and optimal path of tether's in-plane swing angle, tether's in-plane swing angular velocity, main satellite pitching angle, main satellite pitching angular velocity and tether speed

    表  1  绳系系统参数

    Table  1.   Parameters of tethered system

    参数 数值
    主星发动机推力/N 100
    主星质量/kg 100
    主星惯量/(kg·m2) 166.67
    拖拽目标质量/kg 8
    系绳未拉伸长度/m 200
    下载: 导出CSV
  • [1] 朱仁璋, 雷达, 林华宝.绳系卫星系统复杂模型研究[J].宇航学报, 1999, 20(3):7-12. doi: 10.3321/j.issn:1000-1328.1999.03.002

    ZHU R Z, LEI D, LING H B.A sophisticated dynamical model of tethered satellite systems[J]. Journal of Astronautics, 1999, 20(3):7-12(in Chinese). doi: 10.3321/j.issn:1000-1328.1999.03.002
    [2] 钟睿, 徐世杰.基于直接配点法的绳系卫星系统变轨控制[J].航空学报, 2010, 31(3):572-578. http://d.old.wanfangdata.com.cn/Periodical/hkxb201003020

    ZHONG R, XU S J.Orbit-transfer control for TSS using direct collocation method[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(3):572-578(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/hkxb201003020
    [3] XU W, LIANG B, GAO D, et al.A space robotic system used for on-orbit servicing in the geostationary orbit[C]//Proceedings of 2010 International Conference on Intelligent Robots and Systems.Piscataway, NJ: IEEE Press, 2010: 4089-4094.
    [4] MANKALA K K, AGRAWAL S K.Dynamic modeling and simulation of impact in tether net/gripper systems[J]. Multibody System Dynamics, 2004, 11(3):235-250. doi: 10.1023/B:MUBO.0000029393.25494.64
    [5] 刘海涛, 杨乐平, 张青斌, 等.地球静止轨道废弃卫星绳系拖曳离轨研究[J].中国科学:技术科学, 2012, 42(7):780-787. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=QK201201773473

    LIU H T, YANG L P, ZHANG Q B, et al.An investigation on tether-tugging de-orbit of defunct geostationary satellites[J]. Scientia Sinica Technologica, 2012, 42(7):780-787(in Chinese). http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=QK201201773473
    [6] ZHAI G, ZHANG J, YAO Z.Circular orbit target capture using space tether-net system[J]. Mathematical Problems in Engineering, 2013, 2013(4):87-118. http://d.old.wanfangdata.com.cn/OAPaper/oai_doaj-articles_cb213b98c7d597b65daf3817e02eafb2
    [7] QI R, MISRA A K, ZUO Z.Active debris removal using double-tethered space-tug system[J]. Journal of Guidance, Control, and Guidance, 2016, 40(3):1-9.
    [8] WILLIAMS P.Optimal control of a tethered payload capture maneuver[C]//41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston: AIAA, 2005: 1-23.
    [9] WEN H, JIN D P, HU H Y.Infinite-horizon control for retrieving a tethered subsatellite via an elastic tether[J]. Journal of Guidance, Control, and Dynamics, 2008, 31(4):899-906. doi: 10.2514/1.33224
    [10] 王晓宇, 金栋平.计入姿态的绳系卫星概周期振动[J].振动工程学报, 2010, 23(4):361-365. doi: 10.3969/j.issn.1004-4523.2010.04.001

    WANG X Y, JIN D P.Quasi-periodic oscil lation of a tethered subsatell ite with attitude[J]. Journal of Vibration Engineering, 2010, 23(4):361-365(in Chinese). doi: 10.3969/j.issn.1004-4523.2010.04.001
    [11] ZHAO G W, TANG B, SUN L, et al.Effect and control of pendular motion of abandoned satellite on tether drag system[J]. Applied Mechanics & Materials, 2014, 513-517:3900-3906.
    [12] 赵国伟, 张兴民, 唐斌, 等.空间绳系拖拽系统摆动特性与平稳控制[J].北京航空航天大学学报, 2016, 42(4):694-702. http://bhxb.buaa.edu.cn/CN/abstract/abstract13863.shtml

    ZHAO G W, ZHANG X M, TANG B, et al.Properties of pendulum motion of tether tugging system and its stable control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(4):694-702(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract13863.shtml
    [13] QIN S J, BADGWELL T A.A survey of industrial model predictive control technology[J]. Control Engineering Practice, 2003, 11(7):733-764. doi: 10.1016/S0967-0661(02)00186-7
    [14] 席裕庚, 李德伟, 林姝.模型预测控制——现状与挑战[J].自动化学报, 2013, 39(3):222-236. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=QKC20132013040900031996

    XI Y G, LI D W, LIN S.Model predictive control-Status and challenges[J]. Acta Automatica Sinica, 2013, 39(3):222-236(in Chinese). http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=QKC20132013040900031996
    [15] 范国伟, 常琳, 戴路, 等.敏捷卫星姿态机动的非线性模型预测控制[J].光学精密工程, 2015, 23(8):2318-2327. http://d.old.wanfangdata.com.cn/Periodical/gxjmgc201508026

    FAN G W, CHANG L, DAI L, et al.Nonlinear model predictive control of agile satellite attitude maneuver[J]. Optics and Precision Engineering, 2015, 23(8):2318-2327(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/gxjmgc201508026
    [16] LAKSHMANAN P K, MODI V J, MISRA A K.Dynamics and control of the tethered satellite system in the presence of offsets[J]. Acta Astronautica, 1987, 15(12):1053-1057. doi: 10.1016/0094-5765(87)90031-2
    [17] ZHONG R, ZHU Z H.Timescale separate optimal control of tethered space-tug systems for space-debris removal[J]. Journal of Guidance, Control, and Dynamics, 2016, 39(11):2540-2545. doi: 10.2514/1.G001867
    [18] 徐少兵, 李升波, 成波.最优控制问题的Legendre伪谱法求解及其应用[J].控制与决策, 2014, 29(12):2113-2120. http://d.old.wanfangdata.com.cn/Periodical/kzyjc201412001

    XU S B, LI S B, CHENG B.Theory and application of Legendre pseudo-spectral method for solving optimal control problem[J]. Control and Decision, 2014, 29(12):2113-2120(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/kzyjc201412001
    [19] 孙银健.基于模型预测控制的无人驾驶车辆轨迹跟踪控制算法研究[D].北京: 北京理工大学, 2015. http://cdmd.cnki.com.cn/Article/CDMD-10007-1015030238.htm

    SUN Y J.Research on model predictive control-based trajectory tracking algorithm for unmanned vehicles[D]. Beijing: Beijing Institute of Technology, 2015(in Chinese). http://cdmd.cnki.com.cn/Article/CDMD-10007-1015030238.htm
    [20] 陈薇.非线性预测控制快速算法的研究与应用[D].合肥: 中国科学技术大学, 2007. http://cdmd.cnki.com.cn/article/cdmd-10358-2007097280.htm

    CHEN W.Study and application of nonlinear model predictive control fast algorithm[D]. Hefei: University of Science and Technology of China, 2007(in Chinese). http://cdmd.cnki.com.cn/article/cdmd-10358-2007097280.htm
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出版历程
  • 收稿日期:  2018-01-02
  • 录用日期:  2018-03-30
  • 刊出日期:  2018-10-20

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