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结构偏差对二维连续地月载荷转移系统动力学影响

齐乃明 阳勇 黄盘兴 孙康 韩冰

齐乃明, 阳勇, 黄盘兴, 等 . 结构偏差对二维连续地月载荷转移系统动力学影响[J]. 北京航空航天大学学报, 2015, 41(11): 2000-2009. doi: 10.13700/j.bh.1001-5965.2014.0730
引用本文: 齐乃明, 阳勇, 黄盘兴, 等 . 结构偏差对二维连续地月载荷转移系统动力学影响[J]. 北京航空航天大学学报, 2015, 41(11): 2000-2009. doi: 10.13700/j.bh.1001-5965.2014.0730
QI Naiming, YANG Yong, HUANG Panxing, et al. Two dimensional dynamics of continuous cislunar payload transfer system considering structural deviation effect[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11): 2000-2009. doi: 10.13700/j.bh.1001-5965.2014.0730(in Chinese)
Citation: QI Naiming, YANG Yong, HUANG Panxing, et al. Two dimensional dynamics of continuous cislunar payload transfer system considering structural deviation effect[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11): 2000-2009. doi: 10.13700/j.bh.1001-5965.2014.0730(in Chinese)

结构偏差对二维连续地月载荷转移系统动力学影响

doi: 10.13700/j.bh.1001-5965.2014.0730
基金项目: CAST重点创新基金(CAST20090801)
详细信息
    通讯作者:

    齐乃明(1962-),男,黑龙江哈尔滨人,教授,qinmok@163.com,主要研究方向为空间飞行器动力学、机电一体化.

  • 中图分类号: V476.3

Two dimensional dynamics of continuous cislunar payload transfer system considering structural deviation effect

  • 摘要: 以驱动型动量交换绳系卫星系统(MMET)为载体,采用动量交换原理,考虑母星两端系绳长度偏差、两载荷质量偏差等结构偏差的前提下,应用拉格朗日(Lagrange)方法建立了连续地月载荷转移系统(CCPTS)的二维误差动力学模型.在不同的系绳长度偏差以及载荷质量偏差前提下,对所建立的误差动力学模型进行了数值仿真分析.仿真结果表明,系绳长度偏差以及载荷质量偏差对CCPTS的广义坐标、广义速度等动力学参数均产生了相似的影响,随着系绳长度偏差的增加(或载荷质量偏差的增加),CCPTS的广义坐标、广义速度偏差量的最大值均呈现相同的线性增加趋势,而对于广义加速度而言,则没有明显的线性关系.外力矩的存在能够在一定程度上削减因结构偏差所造成的对CCPTS动力学参数的影响程度.

     

  • [1] Carrou J A.Guidebook for analysis of tether applications, NASA-CR-178903[R].Washington D.C.:NASA, 1985.
    [2] Chen Y, Huang R, He L P, et al.Dynamical modelling and control of space tethers:A review of space tether research[J].Nonlinear Dynamics, 2014, 77(4):1077-1099.
    [3] George A K.Advantages of tether release of satellites from elliptic orbits[J].Journal of Guidance, Control, and Dynamics, 1988, 11(5):441-448.
    [4] Zhong L, Peter M B.Momentum exchange:Feedback control of flexible spacecraft maneuvers and vibration[J].Journal of Guidance, Control, and Dynamics, 1992, 15(6):1354-1361.
    [5] Puig-Suari J, Longuski J M, Tragesser S G.A tether sling for lunar and interplanetary exploration[J].Acta Astronautica, 1995, 36(6):291-295.
    [6] Chernousko F L.Dynamics of retrieval of a space tethered system[J].Journal of Application Mathematics and Mechanics, 1995, 59(2):165-173.
    [7] Maximilian M S, Ryan P R.Jovian orbit capture and eccentricity reduction using electrodynamic tether propulsion[J].Journal of Spacecraft and Rockets, 2015, 52(2):506-516.
    [8] Robert P H, Chauncey U.Cislunar tether transport system[J].Journal of Spacecraft and Rockets, 2000, 37(2):177-186.
    [9] Cartmell M P.Generating velocity increments by means of a spinning motorised tether[J].AIAA Journal, 1998, 21(2):155-158.
    [10] Cartmell M P, McKenzie D J.A review of space tether research[J].Progress in Aerospace Science, 2007, 44(1):1-22.
    [11] Ziegler S W.The rigid body dynamic of tethers in space[D].Glasgow:University of Glasgow, 2003.
    [12] Ziegler S W, Cartmell M P.Using motorized tethers for payload orbital transfer[J].Journal of Spacecraft and Rockets, 2001, 38(6):904-913.
    [13] Chen Y.Dynamical modelling of a flexible motorised momentum exchange tether and hybrid fuzzy sliding mode control for spin-up[D].Glasgow:University of Glasgow, 2010.
    [14] Chen Y, Cartmell M P.Hybrid fuzzy sliding mode control for motorised space tether spin-up when coupled with axial and torsional oscillation[J].Astrophys Space Science, 2010, 326(1):105-118.
    [15] Ismail N A.The dynamics of a flexible motorised momentum exchange tether (MMET)[D].Glasgow:University of Glasgow, 2012.
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出版历程
  • 收稿日期:  2014-11-21
  • 修回日期:  2015-02-25
  • 网络出版日期:  2015-11-20

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