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单向执行器系统配置的完整性 被引量:1

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摘要 本文提出了单向执行器系统配置完整性的概念,用来表征其控制作用生成能力。并从一般意义下,讨论了配置矩阵的完整性问题,给出了配置矩阵完整性的若干性质和一些判别方法。存在个别执行器失效时,引入了完整度的概念用以评价配置的容错性能,并给出其判别方法。
作者 张兵 吴宏鑫
出处 《控制工程(北京)》 1998年第4期6-13,共8页
基金 国家自然科学基金和863课题资助
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参考文献5

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同被引文献12

  • 1Doman D B,Gamble B J,Ngo A D.Quantized control allocation of reaction control jets and aerodynamic control surfaces[J].J of Guidance,Control,and Dynamics,2009,32(1):13-24.
  • 2Peter J W.Minimum control authority plot:A tool for designing thruster systems[J].J of Guidance,Control,and Dynamics,1994,17(5):998-1006.
  • 3Crawford B S.Configuration design and efficient operation of redundant multi-jet systems[C].Proc of AIAA Guidance Control and Flight Mechanics Conf.Princeton:AIAA Press,1969.
  • 4张兵.反应作用控制系统容错控制方法研究及应用[D].北京:中国空间技术研究院,1998:42-51.
  • 5Ankersen F,Wu S F.Optimization of spacecraft thruster management function[J].J of Guidance,Control,and Dynamics,2005,28(6):1283-1290.
  • 6Pablo A S.Control allocation for gimbaled/fixed thrusters[J].Acta Astronautica,2010,66(3/4):587-594.
  • 7Jin H P,Wiktor P,DeBra D B.An optimal thruster configuration design and evaluation for quick step[J].Control Engineering Practice,1995,3(8):1113-1118.
  • 8Hwang T W.Upper-stage launch vehicle servo controller design considering optimal thruster configuration[C].Proc of AIAA Guidance,Navigation,and Control Conf and Exhibit.Austin:AIAA Press,2003.
  • 9Bard S C.Configuration design and efficient operation of redundant multi-jet systems[C].Proc of AIAA Guidance Control and Flight Mechanics Conf.Princeton:AIAA Press,1969.
  • 10Pablo A S,Ricardo S S P.Thruster design for position/attitude control of spacecraft[J].IEEE Trans on Aerospace and Electronic Systems,2002,38(4):1172-1179.

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