用户名: 密码: 验证码:
视觉导引受限下空间绳系机器人最优逼近控制
详细信息    查看全文 | 推荐本文 |
  • 英文篇名:Optimal Control of Approaching Target for a Tethered Space Robot under Constraint of Vision Guidance
  • 作者:胡永新 ; 黄攀峰 ; 孟中杰 ; 刘正雄 ; 张夷斋 ; 董刚奇
  • 英文作者:HU Yong-xin;HUANG Pan-feng;MENG Zhong-jie;LIU Zheng-xiong;ZHANG Yi-zhai;DONG Gang-qi;Research Center for Intelligent Robotics, School of Astronautics, Northwestern Polytechnical University;National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University;
  • 关键词:空间绳系机器人 ; 目标逼近 ; 高斯伪谱法 ; 最优控制
  • 英文关键词:Tethered space robot;;Approaching target;;Gaussian pseudospectral method;;Optimal control method
  • 中文刊名:YHXB
  • 英文刊名:Journal of Astronautics
  • 机构:西北工业大学航天学院智能机器人研究中心;西北工业大学航天飞行动力学技术国家重点实验室;
  • 出版日期:2019-04-30
  • 出版单位:宇航学报
  • 年:2019
  • 期:v.40
  • 基金:国家杰出青年科学基金(61725303);; 国家自然科学基金(61773317,61603359);; 中央高校基本科研业务费(3102017jg02005,3102018JGC001)
  • 语种:中文;
  • 页:YHXB201904007
  • 页数:10
  • CN:04
  • ISSN:11-2053/V
  • 分类号:51-60
摘要
针对空间绳系机器人对目标逼近过程中单目视觉视线角约束和导航信息不全问题,首先建立空间绳系机器人系统动力学模型。然后考虑抓捕器视线角约束,采用高斯伪谱法对空间绳系机器人逼近任务姿轨轨迹进行一体规划。同时设计无需相对目标距离的闭环控制器实现对空间绳系机器人最优姿轨轨迹进行跟踪控制。仿真结果表明,该方案能够克服视觉导引受限的影响,实现空间绳系机器人对位姿最优轨迹的精确跟踪。
        Aiming to the problem of the incomplete navigation information and constraint of line-of-sight angle during the target approaching phase for a tethered space robot, the dynamic model of the tethered space robot is established. Considering the constraints of the control inputs and the field of view of the gripper, the optimal approaching trajectory of the tethered space robot to the target is designed using the Gaussian pseudospectral method. A closed loop optimal control scheme is presented without using the relative distance between the gripper and the target. The simulation results of the closed-loop control scheme show that the proposed scheme can overcome the influence of the constraint of line-of-sight angle and realize the accurate position and attitude tracking of the optimal trajectory.
引文
[1] 孟中杰,黄攀峰.空间绳系机器人飞行控制技术[M].北京:中国宇航出版社,2018.
    [2] Huang P F,Zhang F,Cai J,et al.Dexterous tethered space robot:design,measurement,control and experiment[J].IEEE Transactions on Aerospace and Electronic Systems,2017,53(6):1452-1468.
    [3] Zhang F,Huang P F.Releasing dynamics and stability control of maneuverable tethered space net[J].IEEE/ASME Transactions on Mechatronics,2017,22(2):983-993.
    [4] Meng Z J,Huang P F,Guo J.Approach modeling and control of an autonomous maneuverable space net[J].IEEE Transactions on Aerospace and Electronic Systems,2017,53(6):2651-2661.
    [5] Huang P F,Wang D K,Zhang F,et al.Postcapture robust nonlinear control for tethered space robot with constraints on actuator and velocity of space tether[J].International Journal Robust Nonlinear Control,2017,27(16):2824-2841.
    [6] Huang P F,Wang D K,Meng Z J,et al.Adaptive postcapture backstepping control for tumbling tethered space robot-target combination[J].Journal of Guidance,Control and Dynamics,2016,39(1):150-156.
    [7] 黄攀峰,孟中杰.空间绳系机器人技术[M].北京:中国宇航出版社,2014:91-139.
    [8] Yu B S,Jin D P,Wen H.Analytical deployment control law for a flexible tethered satellite system[J].Aerospace Science and Technology,2017,66:294-303.
    [9] Qi R,Misra A K,Zuo Z Y.Active debris removal using double-tethered space-tug system[J].Journal of Guidance,Control and Dynamics,2016,40(3):722-730.
    [10] Zhang J R,Yang K Y,Qi R.Dynamics and offset control of tethered space-tug system[J].Acta Astronautica,2018,142:232-252.
    [11] William J O,Deborah J H.Detumbling of space debris by a net and elastic tether[J].Journal of Guidance,Control and Dynamics,2017,40(7):1829-1836.
    [12] Lu Y B,Huang P F,Meng Z J,et al.Finite time attitude takeover control for combination via tethered space robot[J].Acta Astronautica,2017,136:9-21.
    [13] Zhai G,Zheng H M,Zhang B.Observer-based control for the platform of a tethered space robot[J].Chinese Journal of Aeronautics,2018:1-10.
    [14] Chu Z Y,Di J N,Cui J.Analysis of the effect of attachment point bias during large space debris removal using a tethered space tug[J].Acta Astronautica,2017,139:34-41.
    [15] Wen H,Zhu Z H,Jin D P,et al.Constrained tension control of a tethered space-tug system with only length measurement[J].Acta Astronautica,2016,119:110-117.
    [16] Wang B H,Meng Z J,Huang P F.Attitude control of towed space debris using only tether[J].Acta Astronautica,2017,138:152-167.
    [17] Chen L,Huang P F,Cai J,et al.A non-cooperative target grasping position prediction model for tethered space robot[J].Aerospace Science and Technology,2016,58:571-581.
    [18] Hu Y X,Huang P F,Meng Z J,et al.Approaching control for tethered space robot based on disturbance observer using super twisting law[J].Advances in Space Research,2018,61(9):2344-2351.
    [19] 孟中杰,蔡佳,胡仄虹,等.空间绳系机器人超近距视觉伺服控制方法[J].宇航学报,2015,36(1):40-46.[Meng Zhong-jie,Cai Jia,Hu Ze-hong,et al.A short-distance visual servo control method for the tethered space robot system[J].Journal of Astronautics,2015,36(1):40-46.]
    [20] Botta E M,Sharf I,Misra A K.Contact dynamics modeling and simulation of tether nets for space-debris capture[J].Journal of Guidance,Control,and Dynamics,2016:110-123.
    [21] 黄攀峰,胡永新,王东科,等.空间绳系机器人目标抓捕鲁棒自适应控制器设计[J].自动化学报,2017,43(4):538-547.[Huang Pan-feng,Hu Yong-xin,Wang Dong-ke,et al.Capturing target for tethered space robot using robust adaptive controller[J].Acta Automatica Sinica,2017,43(4):538-547.]
    [22] Wang D K,Huang P F,Cai J,et al.Coordinated control of tethered space robot using mobile tether attachment point in approaching phase[J].Advances in Space Research,2014,54(6):1077-1091.
    [23] Zhang Y Z,Huang P F,Meng Z J,et al.Precise angles-only navigation for noncooperative proximity operation with applicationto tethered space robot[J].IEEE Transactions on Control Systems Technology,2018 (99):1-12.
    [24] Hughes P C.Spacecraft attitude dynamics [M].New Jersey:John Wiley & Sons,Inc,1986.
    [25] Soltani M,Keshmiri M,Misra A K.Dynamic analysis and trajectory tracking of a tethered space robot[J].Acta Astro-nautica,2016,128:335-342.
    [26] Betts J T.Survey of numerical methods for trajectory optimization[J].Journal of Guidance,Control,and Dynamics,1998,21(2):193-207.
    [27] Chu X Y,Zhang J R,Lu S,et al.Optimised collision avoidance for an ultra-close rendezvous with a failed satellite based on the gauss pseudospectral method[J].Acta Astronautica,2016,128:363-376.
    [28] 张志国,余梦伦,耿光有,等.应用伪谱法的运载火箭在线制导方法研究[J].宇航学报,2017,38(3):262-269.[Zhang Zhi-guo,Yu Meng-lun,Geng Guang-you,et al.Research on application of pseudo-spectral method in online guidance method for a launch vehicle[J].Journal of Astro-nautics,2017,38(3):262-269.]
    [29] 白瑞光,孙鑫,陈秋双,等.基于Gauss伪谱法的多UAV协同航迹规划[J].宇航学报,2014,35(9):1022-1029.[Bai Rui-guang,Sun Xin,Chen Qiu-shuang,et al.Multiple UAV cooperative trajectory planning based on gauss pseudospectral method[J].Journal of Astronautics,2014,35(9):1022-1029.]

© 2004-2018 中国地质图书馆版权所有 京ICP备05064691号 京公网安备11010802017129号

地址:北京市海淀区学院路29号 邮编:100083

电话:办公室:(+86 10)66554848;文献借阅、咨询服务、科技查新:66554700