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Deployment and retrieval of tethered satellite system under J_2 perturbation and heating effect

机译：J_2摄动和热效应下的束缚卫星系统的部署和检索

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摘要

Tethered satellite system is subject to a variety of perturbations from the geophysical environment and other planets, such as the J_2 perturbation and heating effect. Those perturbations are likely to yield new dynamics of tethered satellite system during deployment and retrieval. However, the J_2 perturbation and heating effect in studying the deployment and retrieval of tethered satellite have drawn little attention. This paper presents the effect of J_2 perturbation on the deployment and retrieval of tethered satellite and gives the new dynamics with the heating effect taken into account. The viscoelastic tether is modeled as a series of elements with lumped masses, which yields a set of ordinary differential equations of motion having finite degrees of freedom by using Newton's laws. The forces on the system are on the basis of the J_2 perturbation and the thermal flux arising from the solar radiation, Earth's infrared radiation as well as tether's infrared radiation. The case studies show that the J_2 perturbation has a great influence on the deployment process, which depends mainly on the magnitude of sliding friction force between tether and deployment device. The heating effect, however, gives rise to quite different dynamics during retrieval of a tethered satellite compared with that of a tethered satellite without heating effect.
机译：系留卫星系统受到地球物理环境和其他行星的各种扰动，例如J_2扰动和热效应。这些干扰可能会在部署和检索过程中产生拴系卫星系统的新动态。然而，在研究束缚卫星的部署和回收过程中，J_2的摄动和热效应引起了人们的关注。本文介绍了J_2扰动对系留卫星的部署和取回的影响，并考虑了加热效应，给出了新的动力学。粘弹性系绳建模为一系列具有集总质量的元素，这通过使用牛顿定律产生了一组具有有限自由度的常微分运动方程。系统上的力是基于J_2扰动以及太阳辐射，地球的红外辐射以及系绳的红外辐射产生的热通量。案例研究表明，J_2扰动对展开过程有很大影响，这主要取决于系绳与展开装置之间的滑动摩擦力的大小。然而，与没有加热效果的系留卫星相比，加热效果在系留卫星的取回过程中产生了截然不同的动力学。

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  • 来源
    《Acta astronautica》 |2010年第8期|P.845-853|共9页
  • 作者

    B.S. Yu; rnD.P. Jin;

  • 作者单位

    Institute of Vibration Engineering Research, MOE Key Lab of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, PR China;

    rnInstitute of Vibration Engineering Research, MOE Key Lab of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, PR China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    tethered satellite system; deployment and retrieval; J_2 perturbation; heating effect;

    机译：系留卫星系统;部署和检索;J_2摄动;加热效果;

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