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Experimental Verification of Periodic Libration of Tethered Satellite System in Elliptic Orbit

机译：椭圆轨道拴系卫星系统周期振动的实验验证

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摘要

Tethered satellite systems are often considered as revolutionary new technologies capable of solving complex tasks for challenging future space missions such as construction of large space structures, momentum exchange [1], debris elimination [2], artificial gravity generation by rotational motion, and so on [3]. To make the application of tethered satellite systems feasible, their dynamics and control must be comprehensively understood and properly addressed. In the past, ground-based experimental setups have been constructed to study dynamics and control of tethered satellite systems experimentally. In particular, a case of a tethered subsatellite retrieval to and deployment from the mother satellite in circular orbits has been considered in detail [4,5].
机译：拴系卫星系统通常被认为是革命性的新技术，能够解决挑战性未来太空任务的复杂任务，例如大型空间结构的建造，动量交换[1]，碎屑消除[2]，通过旋转运动产生人工重力等。 [3]。为了使系留卫星系统的应用可行，必须全面了解并适当解决其动力学和控制问题。过去，已经建立了基于地面的实验装置来通过实验研究系留卫星系统的动力学和控制。特别是，已经详细考虑了将束缚式亚卫星检索到圆形轨道中的母卫星并从其部署的情况[4,5]。

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    《Journal of guidance, control, and dynamics》 |2011年第2期|p.614-618|共5页
  • 作者

    Hirohisa Kojima; Yoshiyasu Furukawa; Pavel M. Trivailo;

  • 作者单位

    Tokyo Metropolitan University, Hino, Tokyo 191-0065, Japan Department of Aerospace Engineering;

    Tokyo Metropolitan University, Hino, Tokyo 191-0065, Japan Department of Aerospace Engineering;

    Royal Melbourne Institute of Technology, Melbourne, Victoria 3083, Australia School of Aerospace, Mechanical, and Manufacturing Engineering;

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