失效卫星在轨消旋接触控制研究
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- 英文论文题名：Research on Dynamics and Control of On-Orbit Disabled Satellites for positive tumbling breaking
- 论文作者：段文杰 ; 朱志斌 ; 徐拴锋
- 英文论文作者：Duan Wenjie ; Zhu Zhibin ; Xu Shuanfeng ; Beijing Institute of Control Engineering ; Science and Technology on Space Intelligent Control Laboratory
- 年：2017
- 作者机构：北京控制工程研究所;空间智能控制技术重点实验室;
- 论文关键词：抓捕 ; 消旋 ; 卫星
- 英文论文关键词：Capturing ; tumbling breaking ; satellite
- 会议召开时间：2017-07-26
- 会议录名称：第36届中国控制会议论文集（A）
- 英文会议录名称：Proceedings of the 36th Chinese Control Conference（A）
- 语种：中文
- 分类号：V448.2
- 学会代码：KZLL
- 会议名称：第36届中国控制会议
- 会议地点：中国辽宁大连
- 主办单位：中国自动化学会控制理论专业委员会
- 学会名称：中国自动化学会控制理论专业委员会
- 页数：6
- 文件大小：528k
- 原文格式：D
- 会议级别：全国
摘要
对于几°/s到几十°/s高速旋转的失效卫星,除了定轴转动,还可能附带章动,对导航测量以及抓捕任务带来了很大困难,对失效进行主动消旋降低其自旋角速度是对高速旋转目标成功抓捕的首要条件。本文研究对象是带柔性杆制成刷子的主动消旋卫星和带帆板的失效卫星,刷子与失效卫星的帆板接触,接触力由柔性杆的弯曲变形产生,包括接触对之间的压力和摩擦力。接触力可以降低失效卫星的自旋角速度达到给失效卫星消旋的目的。文中建立了接触动力学,基于接触动力学给出了前馈与反馈结合的控制方法,给出了仿真算例。
For disabled satellites tumbling at high speed(several or dozens of°/s), the movement can usually be divided into two parts, i.e.,the spinning around a fixed axis and the nutation, where the latter introduces challenge for guidance measurement and capturing task. The principal condition for capturing is to perform positive tumbling breaking such that the spinning velocity is reduced to the acceptable range. In this paper, we consider positive tumbling breaking satellites with flexible-link brushes. The contact force between the brush and the satellite includes the flexible force due to bend transform and the friction, which is utilized to achieve tumbling breaking by reducing the spinning velocity. Contact dynamics feedback and feedforword control is set up. Simulation of the contact problem is conducted.
For disabled satellites tumbling at high speed(several or dozens of°/s), the movement can usually be divided into two parts, i.e.,the spinning around a fixed axis and the nutation, where the latter introduces challenge for guidance measurement and capturing task. The principal condition for capturing is to perform positive tumbling breaking such that the spinning velocity is reduced to the acceptable range. In this paper, we consider positive tumbling breaking satellites with flexible-link brushes. The contact force between the brush and the satellite includes the flexible force due to bend transform and the friction, which is utilized to achieve tumbling breaking by reducing the spinning velocity. Contact dynamics feedback and feedforword control is set up. Simulation of the contact problem is conducted.
引文
[1]S.Matunaga,et al.Rotational motion-damper for the capture of an uncontrolled floating satellite.In J.of Control Engineering Practice,vol.9,pp.199–205,2001.
[2]Fumihito Sugai,Satoko Abiko,Teppei Tsujita,Xin Jiang,and Masaru Uchiyama.Detumbling an Uncontrolled Satellite with Contactless Force by Using an Eddy Current Brake.In Proc.2013 IEEE/RSJ International Conference on Intelligent Robots and Systems(IROS)November 3-7,Tokyo,Japan,2013.
[3]Shin-Ichiro Nishida and Satomi Kawamoto.Dynamical Simulations for Space Debris Capture.SICE Annual Conference 2011 September 13-18,2011,Waseda University,Tokyo,Japan,pp.2283-2286.
[4]Albert Caubet,James D.Biggs.Design of an Attitude Stabilization Electromagnetic Module for Detumbling Uncooperative Targets.In Proc.Aerospace Conference,2014 IEEE.
[5]Biele,S.Ulamec.Capabilities of Philae,the Rosetta Lander.Space Sci Rev 138:275–289,2008.
[6]Fares C Hamam Y Collision detection for rigid bodies A state of the art review[J]Graphi Con 2005 2005
[2]Fumihito Sugai,Satoko Abiko,Teppei Tsujita,Xin Jiang,and Masaru Uchiyama.Detumbling an Uncontrolled Satellite with Contactless Force by Using an Eddy Current Brake.In Proc.2013 IEEE/RSJ International Conference on Intelligent Robots and Systems(IROS)November 3-7,Tokyo,Japan,2013.
[3]Shin-Ichiro Nishida and Satomi Kawamoto.Dynamical Simulations for Space Debris Capture.SICE Annual Conference 2011 September 13-18,2011,Waseda University,Tokyo,Japan,pp.2283-2286.
[4]Albert Caubet,James D.Biggs.Design of an Attitude Stabilization Electromagnetic Module for Detumbling Uncooperative Targets.In Proc.Aerospace Conference,2014 IEEE.
[5]Biele,S.Ulamec.Capabilities of Philae,the Rosetta Lander.Space Sci Rev 138:275–289,2008.
[6]Fares C Hamam Y Collision detection for rigid bodies A state of the art review[J]Graphi Con 2005 2005