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Advances in dynamics and control of tethered satellite systems

         

摘要

The concept of tethered satellite system (TSS) promises to revolutionize many aspects of space exploration and exploitation. It provides not only numerous possible and valuable applications, but also challenging and interesting problems related to their dynamics, control, and physical implementation. Over the past decades, this exciting topic has attracted significant attention from many researchers and gained a vast number of analytical, numerical and experimental achievements with a focus on the two essential aspects of both dynamics and control. This review article presents the historic background and recent hot topics for the space tethers, and introduces the dynamics and control of TSSs in a progressive manner, from basic operating principles to the state-of-the-art achievements.

著录项

  • 来源
    《力学学报:英文版》 |2008年第003期|229-241|共13页
  • 作者单位

    MOE Key Lab of Structure Mechanics and Control for Aircraft, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, China;

    MOE Key Lab of Structure Mechanics and Control for Aircraft, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, China;

    MOE Key Lab of Structure Mechanics and Control for Aircraft, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, China;

  • 原文格式 PDF
  • 正文语种 chi
  • 中图分类 力学;
  • 关键词

    Tethered satellite system; Space tether; Dynamics; Control;

    机译:系留卫星系统;太空系绳;动力学;控制;
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