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空间绳系机器人逼近目标协调控制方法
引用本文:徐秀栋,黄攀峰,孟中杰.空间绳系机器人逼近目标协调控制方法[J].航空学报,2013,34(5):1222-1231.
作者姓名:徐秀栋  黄攀峰  孟中杰
作者单位:西北工业大学航天飞行动力学技术重点实验室,陕西西安,710072
基金项目:西北工业大学博士论文创新基金,国家自然科学基金,航天飞行动力学技术重点实验室开放基金
摘    要: 为了节省空间绳系机器人的末端执行装置在逼近目标卫星过程中推力器所使用的燃料,本文提出一种利用推力器、反作用轮及空间系绳的协调控制方法。首先利用二次型最优控制器(LQR)算法计算出末端执行装置逼近目标所需的理想轨道控制力,然后利用模拟退火算法将所需轨道控制力优化分配到推力器及空间系绳,同时利用时间延迟算法通过反作用轮补偿空间系绳产生的姿态干扰力矩。仿真结果表明,利用该协调控制方法能显著节省末端执行装置上推力器的燃料消耗,有效抑制空间系绳协调控制力产生的姿态干扰,使末端执行装置保持相对稳定的姿态。

关 键 词:空间绳系机器人  LQR算法  协调控制  模拟退火  时间延迟  

Coordinated Control Method of Space Tethered Robot for Approaching Targets
XU Xiudong , HUANG Panfeng , MENG Zhongjie.Coordinated Control Method of Space Tethered Robot for Approaching Targets[J].Acta Aeronautica et Astronautica Sinica,2013,34(5):1222-1231.
Authors:XU Xiudong  HUANG Panfeng  MENG Zhongjie
Institution:National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi'an 710072, China
Abstract:In order to save the thruster fuel of an end effector for a space tethered robot in the process of approaching a target satellite, a coordinated control method is proposed in the paper which utilizes the thruster, the reaction wheel and the space tether. First, this method calculates the ideal orbit control force of the end effector for the approaching target by linear quadratic regulator (LQR) algorithm. Then this force is allocated to the thrusters and space tether through optimization using a simulated annealing algorithm. Simultaneously, the attitude interferential torque of the space tether is compensated through a reaction wheel using the time delay algorithm. The simulation results show that the coordinated control method can significantly save thruster fuel of the end effector, and it also restrains attitude disturbance produced by the coordinated control force of the space tether and maintains relative attitude stability of the end effector.
Keywords:space tethered robot  LQR algorithm  coordinated control  simulated annealing  time delay
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