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空间碎片绳网捕获拖曳恒张力控制
引用本文:卢山,姜泽华,刘禹.空间碎片绳网捕获拖曳恒张力控制[J].宇航学报,2020,41(7):970-977.
作者姓名:卢山  姜泽华  刘禹
作者单位:1. 上海航天控制技术研究所,上海 201109;2. 上海市空间智能控制技术重点实验室,上海 201109
基金项目:上海市科技人才计划(17XD1420700)
摘    要:针对空间绳网系统捕获空间碎片后,在轨道转移过程中的精确控制问题,提出一种使用常值拉力将空间碎片拖曳至坟墓轨道的方法。首先,采用牛顿欧拉法建立绳系组合体动力学模型;其次,通过李雅普诺夫方法证明仅使用恒张力即可实现拖曳过程的稳定控制;再次,提出采用常值拉力切换控制律抑制空间碎片的姿态章动,采用基于相平面控制原理的控制律抑制绳系组合体面内面外摆动,规避在轨道转移过程中系绳松弛造成缠绕、系绳张力过大造成断裂或两星接近发生碰撞等风险。最后,通过拖曳离轨全过程仿真分析,校验了所提出控制方法的有效性。

关 键 词:空间碎片  绳系系统  牛顿欧拉法  常值拉力  相平面原理  
收稿时间:2019-07-18

Towing Control of Space Debris with Constant Tension
LU Shan,JIANG Ze hua,LIU Yu.Towing Control of Space Debris with Constant Tension[J].Journal of Astronautics,2020,41(7):970-977.
Authors:LU Shan  JIANG Ze hua  LIU Yu
Institution:1. Shanghai Aerospace Control Technology Institute, Shanghai 201109, China; 2. Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai 201109, China
Abstract:A method of towing space debris to the grave orbit by constant tension is proposed for the problem of precise control during orbit transfer. In this paper, the dynamics model of a tethered space-tug (TST) system is firstly formulated by the Newton-Euler method. Then the system stability is proved by the Lyapunov method. The attitude nutation of space debris is restrained by using the constant tension switching control law, and the control law based on the phase plane control principle is proposed to stabilize the in-plane and out-plane swing of the tethered combination, thus preventing the collision between the tug spacecraft and debris as well as the twine and breakage of the tether, and ensuring the safety of the towing process. The numerical simulation shows the effectiveness of the above control methods.
Keywords:Space debris  Tether system  Newton-Euler method  Constant tension  Phase plane principle  
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