Research and development of Tethered Satellite Cluster Systems

被引:0
|
作者
Mori, O [1 ]
Matunaga, S [1 ]
Maeda, N [1 ]
机构
[1] Tokyo Inst Technol, Meguro Ku, Tokyo 1528552, Japan
关键词
D O I
暂无
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this paper, we propose the concept of Tethered Satellite Cluster Systems, as an application of the RoboSat Clusters. The system consists of some satellites joined by tethers, and keeps and changes the constellation Is with tension/length control of the tethers to perform various orbit service missions. We formulate the motion of the system in order to analyze the dynamics and establish the methods of coordinated control of tension and attitude of the satellite, in addition, we develop a ground experiment system including a reel mechanism for the tethered satellite cluster systems. We outline the system components and show results of the fundamental experiments for verification of the reel mechanism and the control method.
引用
收藏
页码:1834 / 1840
页数:7
相关论文
共 50 条
  • [41] Research of Dynamics and Deploying Control Method on Tethered Satellite
    Gang, Lei
    Yong, Xian
    Jie, Feng
    Kui, Wang
    PROCEEDINGS OF INTERNATIONAL CONFERENCE ON SOFT COMPUTING TECHNIQUES AND ENGINEERING APPLICATION, ICSCTEA 2013, 2014, 250 : 63 - 69
  • [42] NONLINEAR FEEDBACK DEPLOYMENT AND RETRIEVAL OF TETHERED SATELLITE SYSTEMS
    KIM, E
    VADALI, SR
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (01) : 28 - 34
  • [43] Deployment/retrieval optimization for flexible tethered satellite systems
    Paul Williams
    Nonlinear Dynamics, 2008, 52 : 159 - 179
  • [44] Review of dynamics and control of nonelectrodynamic tethered satellite systems
    Kumar, K. D.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2006, 43 (04) : 705 - 720
  • [45] 3-DIMENSIONAL VIBRATIONS OF TETHERED SATELLITE SYSTEMS
    PASCA, M
    PIGNATARO, M
    LUONGO, A
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1991, 14 (02) : 312 - 320
  • [46] Deployment/retrieval optimization for flexible tethered satellite systems
    Williams, Paul
    NONLINEAR DYNAMICS, 2008, 52 (1-2) : 159 - 179
  • [47] THEORY OF PLASMA CONTACTORS FOR ELECTRODYNAMIC TETHERED SATELLITE SYSTEMS
    PARKS, DE
    KATZ, I
    JOURNAL OF SPACECRAFT AND ROCKETS, 1987, 24 (03) : 245 - 249
  • [48] Dynamical analysis of the deployment process of tethered satellite systems
    Schagerl, M
    Steindl, A
    Troger, H
    IUTAM-IASS SYMPOSIUM ON DEPLOYABLE STRUCTURES: THEORY AND APPLICATIONS, 2000, 80 : 345 - 354
  • [49] EFFECTS OF AERODYNAMIC LIFT ON THE STABILITY OF TETHERED SATELLITE SYSTEMS
    KESHMIRI, M
    MISRA, AK
    MODI, VJ
    JOURNAL OF THE ASTRONAUTICAL SCIENCES, 1994, 42 (03): : 301 - 318
  • [50] Modeling tethered satellite systems for detection and orbit determination
    Cochran, JE
    Cho, S
    Lovell, TA
    Cicci, DA
    ASTRODYNAMICS 1999, PTS 1-3, 2000, 103 : 1821 - 1841