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Volume 41 Issue 11
Nov.  2015
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Journal of Beijing University of Aeronautics and Astronautics  > 2015  >  41(11): 2000-2009.
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)
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Two dimensional dynamics of continuous cislunar payload transfer system considering structural deviation effect

doi: 10.13700/j.bh.1001-5965.2014.0730

  • School of Astronautics, Harbin Institute of Technology, Harbin 150006, China

  • Received Date: 21 Nov 2014
  • Rev Recd Date: 25 Feb 2015
  • Publish Date: 20 Nov 2015
    Abstract
  • Based on the motorized momentum exchange tether (MMET), with the principle of momentum exchange and by considering the structural deviation (including the tether length deviation and payload mass deviation), the two dimensional error dynamics of continuous cislunar payloads transferring system (CCPTS) was built by Lagrange method and its numerical simulated solution was solved by Mathematica software. Under the conditions of existing the tether length deviation and payload mass deviation, the dynamic simulations of the CCPTS were presented. It is shown that tether length deviation and payload mass deviation have similar influence on CCPTS's dynamics (including generalized coordinates and generalized velocity). With the increment of tether length deviation or payload mass deviation, the maximum of the CCPTS's generalized coordinates' deviation and generalized velocities' deviation increases linearly. However, the maximum of the CCPTS's generalized accelerations have no evident linear relation with the structure deviation of the CCPTS. Lastly, the external torque can weaken the influence degree of the structure deviation of the CCPTS on the dynamic parameters.

     

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    • References(15)
  • [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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