Deployment of a tethered satellite under the action of a braking force

被引：0
|
作者：
Wiedermann, G [1 ]
Steindl, A [1 ]
Troger, H [1 ]
机构：
[1] Vienna Univ Technol, Inst Mech, A-1040 Vienna, Austria
来源：
ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK | 2000年 / 80卷
关键词：
D O I：
暂无
中图分类号：
O29 [应用数学];
学科分类号：
070104 ;
摘要：
Force braked deployment for a system of two satellites in orbit around the earth connected by a thin tether is simulated by means of a Finite Element analysis following the approach proposed in [5].
引用
收藏
页码：S853 / S854
页数：2
相关论文
共 50 条
  • [21] Deployment and retrieval of tethered satellite system under J2 perturbation and heating effect
    Yu, B. S.
    Jin, D. P.
    ACTA ASTRONAUTICA, 2010, 67 (7-8) : 845 - 853
  • [22] Variable Structure Control for Tethered Satellite Fast Deployment and Retrieval
    Liu Yingying
    Zhou Jun
    Chen Huanlong
    2010 INTERNATIONAL COLLOQUIUM ON COMPUTING, COMMUNICATION, CONTROL, AND MANAGEMENT (CCCM2010), VOL IV, 2010, : 395 - 398
  • [23] Deployment strategies for planar multi-tethered satellite formation
    Zhai Guang
    Su Fei
    Zhang Jingrui
    Liang Bin
    AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 71 : 475 - 484
  • [24] A study of the planar deployment dynamics of the ASTOR tethered satellite system
    Mazzoleni, AP
    Coles, RL
    ASTRODYNAMICS 1999, PTS 1-3, 2000, 103 : 1781 - 1799
  • [25] Digital deployment control of a tethered satellite system with constrained tension
    Xu, Shidong
    Chen, Ti
    Wen, Hao
    Jin, Dongping
    ADVANCES IN SPACE RESEARCH, 2023, 72 (10) : 4184 - 4196
  • [26] Analytical deployment control law for a flexible tethered satellite system
    Yu, B. S.
    Jin, D. P.
    Wen, H.
    AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 66 : 294 - 303
  • [27] TETHERED SATELLITE DEPLOYMENT AND RETRIEVAL BY FRACTIONAL ORDER TENSION CONTROL
    Zhu, Zheng H.
    Sun, Guanghui
    SPACEFLIGHT MECHANICS 2015, PTS I-III, 2015, 155 : 3501 - 3508
  • [28] Nonlinear optimal feedback control for deployment/retrieval of a tethered satellite
    Ohtsuka, T
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2001, 43 (142) : 165 - 173
  • [29] Time optimal control for the deployment of a tethered satellite allowing for a massive tether
    Steindl, Alois
    MECCANICA, 2016, 51 (11) : 2741 - 2751
  • [30] Dynamics of variable-length tethers with application to tethered satellite deployment
    Tang, J. L.
    Ren, G. X.
    Zhu, W. D.
    Ren, H.
    COMMUNICATIONS IN NONLINEAR SCIENCE AND NUMERICAL SIMULATION, 2011, 16 (08) : 3411 - 3424
12345