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分布式卫星编队飞行队形保持协同控制 被引量:22

Cooperative Control for Distributed Satellite Formation Keeping
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摘要 针对分布式卫星编队飞行队形保持控制问题提出一种分布式协同控制算法,并给出该协同控制算法与编队卫星星间信息传递拓扑结构之间的关系。该协同控制算法以模型预测控制为基础,利用分布式编队卫星的自然特性以及编队卫星之间的信息传递拓扑结构,采用分布式的算法结构,设计分布式的模型预测协同控制算法。该控制算法是一种在线滚动优化控制算法,同时能够较好地解决存在状态约束、控制输入约束等情形下的各种控制问题。最后通过数值仿真验证了结果的有效性。仿真结果表明,当编队卫星星间信息传递拓扑结构中存在生成树时,提出的分布式协同控制算法能够有效地应用到编队卫星队形保持控制问题上来。 A distributed cooperative control algorithm is proposed in this paper for a class of distributed satellite formation keeping problem,and the relationship between the proposed algorithm and the topology structure of the information communication among foramtion flying satellites is presented.The proposed algorithm is based on model predictive control,and the nature and the topology structure of the distributed satellite formation,are used to design a distributed model predictive control algorithm in a distributed structure.The proposed algorithm is optimized over a finite time on line and can deal with the constrained contol problem well.Numerical simulations have demonstrated the effectiveness of the approach proposed.Simulation results show that the proposed algorithm can be applied to the distributed satellite formation keeping control problem effectively.
出处 《宇航学报》 EI CAS CSCD 北大核心 2011年第10期2140-2145,共6页 Journal of Astronautics
基金 国家自然科学基金(60710002) 机器人技术与系统国家重点实验室自主研究课题(SKLRS200801A03)
关键词 分布式卫星 队形保持 协同控制 分布式模型预测控制 Distributed satellite Formation keeping Cooperative control Distributed model predictive control
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参考文献11

  • 1Olfati S R, Murray R M. Consensus protocols for networks of dynamic agents [ C ]. The 29th American Control Conference, Denver, USA, June 4 - 6, 2003. 被引量:1
  • 2Moreau L. Leaderless coordination via bidirectional and unidirectional time dependent communication [ C ]. The IEEE Conference on Decision and Control, Maui, Hawaii, December 9 - 12, 2003. 被引量:1
  • 3张振民,林来兴.小卫星编队飞行动力学及其应用[J].航天控制,2002,20(3):44-50. 被引量:7
  • 4Jadbabaie A, Lin J, Morse A S. Coordination of groups of mobile autonomous agents using nearest neighbor rules [ J ]. IEEE Transaction on Automatic Control, 2003, 48( 1 ): 988 -1001. 被引量:1
  • 5刘辉,李俊峰.卫星编队飞行的协同控制[J].清华大学学报(自然科学版),2006,46(11):1922-1925. 被引量:7
  • 6Mclain T W, Beard R W. Coordination variables, coordination functions, and cooperative timing missions [ C ]. The 29th American Control Conference, Denver, USA, June 4 -6, 2003. 被引量:1
  • 7Queiroz M S, Kapila V, Yah Q. Adaptive nonlinear control of muhiple spacecraft formation flying [ J ]. Journal of Guidance, Control and Dynamics, 2000, 23 (3) : 385 -390. 被引量:1
  • 8Starin S, Yedavalli R K, Sparks A G. Spacecraft formation flying maneuvers using LQR with no radial axis inputs [C ]. AIAA Guidance, Navigation, and Control Conference, Montreal, Canada, August 6 - 9, 2001. 被引量:1
  • 9Vadali S, Sehaub H, Alfriend K T. Initial conditions and fuel- optimal control for formation flying of satellites[ C]. AIAA Guidance, Navigation, and Control Conference, Portland, USA, August 9 - 12, 1999. 被引量:1
  • 10吴宝林,曹喜滨.基于模型预测的卫星编队队形机动控制[J].吉林大学学报(工学版),2007,37(1):218-223. 被引量:5

二级参考文献18

  • 1林来兴.空间交会对接技术[M].国防工业出版社,1995.. 被引量:21
  • 2Scharf D P,Hadaegh F Y,Ploen S R.A survey of spacecraft formation flying guidance and control (Part Ⅱ):Control[C]∥ Proceedings of American Control Conference.Pasadena:Jet Propulsion Laboratory,NASA,2004:2976-2985. 被引量:1
  • 3Lee D J,Li P Y.Formation and maneuver control for multiple spacecraft[C]∥ Proceedings of American Control Conference.Denver:IEEE,2003:278-283. 被引量:1
  • 4Kapila V,Sparks A G,Buffington J M,et al.Spacecraft formation flying:Dynamic and control[J].J Guidance Control and Dynamics,2000,23(3):561-564. 被引量:1
  • 5Yeh H H,Nelson E,Sparks A.Nonlinear tracking control for satellite formations[J].J Guidance Control and Dynamics,2002,25(2):376-386. 被引量:1
  • 6Wei K,Andy S A,Banda S.Coordinated control of multisatellite systems[J].J Guidance Control and Dynamics,2001,24(2):360-368. 被引量:1
  • 7高云峰.卫星编队飞行相对轨道运动动力学研究[D].北京:清华大学,2001. 被引量:2
  • 8Schaub H,Vadali S R,Junkins J L,et al.Spacecraft formation flying using mean orbit elements[J].Journal of the Astronautical Sciences,2000,48 (1):69-87. 被引量:1
  • 9Vadali S R,Schaub H,Alfriend K T.Initial conditions and fuel-optimal control for formation flying of satellites[C] // AIAA-99-4265. 被引量:1
  • 10Liu lin.Orbit Theory of Spacecraft[M].Beijing:National Defense Industry Press,2000:99-148. 被引量:1

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引证文献22

二级引证文献98

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