Volume 26 Issue 7
Jul.  2011
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LIU Xu-hui, FANG Shu-zhou, LIU Shu-jie, LUO Li, QUAN En. Ignition algorithm of solid propellant micro-thruster array for attitude control[J]. Journal of Aerospace Power, 2011, 26(7): 1659-1664.
Citation: LIU Xu-hui, FANG Shu-zhou, LIU Shu-jie, LUO Li, QUAN En. Ignition algorithm of solid propellant micro-thruster array for attitude control[J]. Journal of Aerospace Power, 2011, 26(7): 1659-1664.

Ignition algorithm of solid propellant micro-thruster array for attitude control

  • Received Date: 2010-06-28
  • Rev Recd Date: 2010-08-23
  • Publish Date: 2011-07-28
  • The study on ignition algorithm of solid propellant micro-thruster array for attitude control of micro-satellite was made and described in this paper.The performance capabilities of solid propellant micro-thruster array were analyzed and the theoretical model was set up,then two kinds of ignition algorithms, that were combined base value algorithm and array programming algorithm, were proposed and verified by simulation using Matlab/Simulink.The simulation shows that, array programming algorithm is accurate and fast, also can improve the utilization efficiency of thrusters in the array.

     

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  • [1]
    Larangot B,Conédéra V,Dubreuil P,et al.Solid propellant microthruster:an alternative propulsion device for nanosatellite //Proceedings of the Conference on Aerospace Energetic Equipment.Avignon France: ,2002:10-19.
    [2]
    Chaalane A,Larang t B,Rossi C,et al.Main directions of solid propellant micro-propulsion activity at LAAS .AIAA Paper 2004-6706,2004.
    [3]
    Kwon S,Lee J,Hoon L D.Design and performance evaluation of components of micro solid propellant thruster .Fort Lauderdale,USA:The 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,2004.
    [4]
    Green A A.Demonstration and quantitative characterization of a MEMS fabricated propulsion system for the next generation of microspacecraft .AIAA-2001-0009,2001.
    [5]
    Zhang K L,Chou S K,Ang S S.Performance prediction of a novel solid-propellant microthruster[J].Journal of Propulsion and Power,2006,22(1):56-63.
    [6]
    Alexeenko A A,Levin D A,Girnelshein S F,et al.Numerical study of flow structure and thrust performance for 3-D MEMS-based nozzles .AIAA-2002-3194,2002.
    [7]
    Wu M H,Yetter R A,Yang V.Development and characterization of ceramic micro chemical propulsion and combustion systems .AIAA-2008-0966,2008.
    [8]
    尤政,张高飞,林杨,等.MEMS 固体化学推进器设计与建模研究[J].光学精密工程,2005,13(2):117-126. YOU Zheng,ZHANG Gaofei,LIN Yang,et al.Design and modeling of MEMS-based solid propellant propulsion[J].Optics and Precision Engineering,2005,13(2):117-126.(in Chinese)
    [9]
    屠善澄.卫星姿态动力学与控制[M].2版.北京:中国宇航出版社,1998:178-179.
    [10]
    Lewis D H,Jr.,Janson S W,Cohen R B,et al.Digital micropropulsion[J].Sensors and Actuators:Physical,2000,80(2):143-156.
    [11]
    章仁为.卫星轨道姿态动力学与控制[M].北京:北京航空航天大学出版社,1997:141-155.
    [12]
    张景瑞.灵敏航天器快速倾斜机动的MCMG参数和力矩估算[J].清华大学学报(自然科学版),2007,47(11):2037-2040. ZHANG Jingrui.Estimation of MCMG parameters and torques for rapid slewing maneuver of agile spacecraft[J].Journal of Tsinghua University(Science and Technology),2007,47(11):2037-2040.(in Chinese)
    [13]
    Rossi C,Do Conto T,Estève D C,et al.Design,fabrication and modelling of MEMS-based microthrusters for space application[J].Smart Materials and Structures,2001,10(6):1156-1162.
    [14]
    李国勇.最优控制理论及参数优化[M].北京:国防工业出版社,2006:118-123.
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