期刊文献+
任意字段
题名或关键词
题名
关键词
文摘
作者
第一作者
机构
刊名
分类号
参考文献
作者简介
基金资助
栏目信息

利用人工势函数法的卫星电磁编队控制 被引量：10

Artificial potential function method for satellite electromagnetic formation control
原文传递
导出
摘要 卫星电磁编队是指利用卫星之间相互作用的电磁力进行卫星相对运动控制,对控制律的要求主要是计算量小和能避免碰撞.以目标星对参考星的相对运动矢量作为控制对象,分析了使用电磁力控制卫星编队的可行性,结果是如果编队卫星磁矩能够任意控制,那么卫星相对运动也能完全控制.设计了人工势函数,以相对位置和相对速度矢量作为变量,人工势函数在达到控制目标时为最小值,在碰撞的位置具有局部最大值.设计的控制律能够实时调整控制参数,能够保证电磁线圈控制电流不至于饱和,以及人工势函数导数在控制过程中小于零.仿真表明,所设计的控制律能生成编队构型并避免碰撞,而且具有一定的抗干扰性. The relative motion of electromagnetic satellites is activated by electromagnetic force between satellites. The control law should satisfy two conditions, low calculation burden and ability of avoiding colli- sion. The control objects are relative motion vectors of satellites to reference satellite. The analysis of feasibili- ty of electromagnetic force control to satellite formation shows that relative motion of satellites can be controlled if electromagnetic strengths of satellites can be controlled. An artificial potential function was designed. Rela- tive positions and relative velocities are treated as variables. The value of the function is minimal when control object is got, and it is local maximal when collision happens. By regulating control parameters in real time, which the current of electromagnetic coils won＇t beyond upper limit is regarded. The derivative of artificial po- tential function is less than zeros in control process. Simulation shows that electromagnetic satellites configura- tion would be generated when control law was imposed with interference.
作者 苏建敏 董云峰
机构地区 北京航空航天大学宇航学院
出处 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2012年第2期213-217,238,共6页 Journal of Beijing University of Aeronautics and Astronautics
关键词 人工势函数 电磁编队 避免碰撞 饱和 抗干扰 artificial potential function electromagnetic formation collision avoidance saturation anti-interference
分类号 V412.4 [航空宇航科学与技术—航空宇航推进理论与工程]
  • 相关文献

参考文献10

  • 1Vaddi S S,Alffiend K T,Vadali S R. Formation establishment and reeonfiguration using impulsive control[ J ]. Journal of Guidance, Control, and Dynamics ,2005,28 (2) :262 - 268.
  • 2He Q, Han C. Dynamics and control of satellite formation flying based on relative orbit elements [ C ]//AIAA Guidance, Navigation and Control Conference and Exhibit. Honolulu :AIAA ,2008.
  • 3Richards A, Schouwenaars T, How J P. Spacecraft trajectory planning with avoidance constraints using mixed-integer linear programming[J]. Journal of Guidance, Control, and Dynamics, 2002,25 (4) :755 - 764.
  • 4Campbell M E. Planning algorithm for multiple satellite clusters [ J ]. Journal of Guidance, Control, and Dynamics ,2003,26 ( 5 ) : 700 - 780.
  • 5Massari M, Zazzera F. Optimization of lowthrust reconfiguration maneuvers for spacecraft flying in formation[J].Journal of Guidance, Control, and Dynamics,2009,32 ( 5 ) : 1629 - 1638.
  • 6张博,罗建军,袁建平.一种基于信息一致性的卫星编队协同控制策略[J].航空学报,2010,31(5):1004-1013. 被引量：13
  • 7Kong E, Kwon D, Schweighart S, et al. Electromagnetic formation flight for multisateUite arrays [ J ] Journal of Spacecraft and Rockets, 2004,41 ( 4 ) :659 - 666.
  • 8Khatib O. Real-time obstacle avoidance for manipulators and mobile robots[J]. The International Journal of Robotics Research, 1986,5 ( 1 ) :90 - 98.
  • 9Martinson N. A new method of guidance control for autonomous rendezvous in a cluttered space environment [C ]//AIAA Guid ance, Navigation, and Control Conference. South Carolina: AIAA ,2007:602 - 610.
  • 10Ahsun U, Miller D. Dynamics and control of electromagnetic satellite formations [D ]. Massachusetts: Department of Aero- nautical and Astronautical Engineerlng, Massachusetts Institute of Technology ,2007.

二级参考文献15

  • 1Randal W B,Jonathan L,Fred Y H.A coordination architecture for spacecraft formation control[J].IEEE Transactions on Control Systems Technology,2001,9(6):777-790.
  • 2Daniel P S,Fred Y H,Scott R P.A survey of spacecraft formation flying guidance and control(Part I):guidance[C] //Proceedings of the American Control Conference.2003:1733-1739.
  • 3Daniel P S,Fred Y H,Scott R P.A survey of spacecraft formation flying guidance and control(Part II):control[C] //Proceedings of the American Control Conference.2003:2976-2985.
  • 4Saber R O,Fax J A,Murray R M.Consensus and cooperation in networked multi-agent systems[J].Proceedings of the IEEE,2007,95(1):215-233.
  • 5Murray R M.Recent research in cooperative control of multi-vehicle systems[C] //International Conference on Advances in Control and Optimization of Dynamical Systems.2007:1-27.
  • 6Wei R,Randal W B,Ella M A.A survey of consensus problems in multi-agent coordination[C] //American Control Conference.2005:1859-1864.
  • 7Wei R,Randal W B,Ella M A.Information consensus in multivehicle cooperative control[J].IEEE Control Systems Magazine,2007,27(2):71-82.
  • 8Wei R,Randal W B.Distributed consensus in multi-vehicle cooperative control theory and application[M].London:Springer Press,2008.
  • 9Wei R.Consensus strategies for cooperative control of vehicle formations[J].IET Control Theory and Applications,2007,1(2):505-512.
  • 10Sorensen N,Wei R.A unified formation control scheme with a single or multiple leaders[C] //Proceedings of the American Control Conference.2007:5412-5418.

共引文献12

同被引文献77

  • 1YANG Yuanxi1 & WEN Yuanlan2 1. Xi’an Research Institute of Surveying and Mapping, Xi抋’an 710054, China,2. College of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073, China.Synthetically adaptive robust filtering for satellite orbit determination[J].Science China Earth Sciences,2004,47(7):585-592. 被引量：24
  • 2林涛,刘永才,关成启,关世义,张克.飞航导弹协同作战使用方法探讨[J].战术导弹技术,2005(2):8-12. 被引量：66
  • 3吴霞,郑建华.基于STK的编队飞行队形保持控制及仿真[J].计算机仿真,2007,24(3):66-68. 被引量：9
  • 4LIU Shi-Cai,TAN Da-Long,LIU Guang-Jun.Robust Leader-follower Formation Control of Mobile Robots Based on a Second Order Kinematics Model[J].自动化学报,2007,33(9):947-955. 被引量：10
  • 5丁溯泉,张波,刘世勇.STK在航天任务仿真分析中的应用[M].北京:国防工业出版社,2011.
  • 6赵育善,师鹏.航天器飞行动力学建模理论与方法[M].北京:北京航空航天大学出版社,2012:23-24.
  • 7Desai J P,Ostrowski J P,Kumar V. Modeling and control of for- mations of nonholonomic mobile robots [ J ]. IEEE Transactions on Robotics and Automation ,2001,17 ( 6 ) :905 - 908.
  • 8Paul T, Krogstad T R, Gravdahl J T. Modelling of UAV formation flight using 3 D potential field [ J ]. Simulation Modelling Practice and Theory ,2008,16 ( 8 ) : 1453 - 1462.
  • 9Semsar E,Khorasani K. Adaptive formation control of UAVs in the presence of unknown vortex forces and leader commands [ C ]//Proceedings of the 2006 American Control Conference. Minneapolis, MN .. IEEE ,2006:3563 - 3568.
  • 10Ren W, Beard R W. Formation feedback control for multiple spacecraft via virtual structures[ J]. lEE Proc Control Theory Ap- pl,2004,151 (3) :357 - 368.

引证文献10

二级引证文献38

北京航空航天大学学报
2012年 第2期

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部