Chaos analysis on librational control of gravity-gradient satellite in elliptic orbit

被引：33
|
作者：
Fujii, HA [1 ]
Ichiki, W [1 ]
Suda, S [1 ]
Watanabe, TR [1 ]
机构：
[1] Tokyo Metropolitan Inst Technol, Dept Aerosp Engn, Hino, Tokyo 1910065, Japan
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2000年 / 23卷 / 01期
关键词：
D O I：
10.2514/2.4500
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The time-delay feedback control (DFC) scheme was applied to the nonlinear dynamics, in particular, the librational motion of gravity-gradient satellites in an elliptic orbit. The DFC scheme was found to be very effective in controlling the chaotic motion by an appropriate utilization of the fundamental characteristics of chaos.
引用
收藏
页码：145 / 146
页数：2
相关论文
共 50 条
  • [21] Hamiltonian and chaotic attitude dynamics of an orbiting gyrostat satellite under gravity-gradient torques
    Kuang, JL
    Leung, AYT
    Tan, S
    PHYSICA D-NONLINEAR PHENOMENA, 2003, 186 (1-2) : 1 - 19
  • [22] COMPLETE CLOSED FORM SOLUTION OF A TUMBLING TRIAXIAL SATELLITE UNDER GRAVITY-GRADIENT TORQUE
    Lara, Martin
    Ferrer, Sebastian
    SPACEFLIGHT MECHANICS 2012, 2012, 143 : 255 - 274
  • [23] Minimum time deployment control for gravity-gradient stabilized space structure
    Kojima, Hirohisa
    Nippon Kikai Gakkai Ronbunshu, C Hen/Transactions of the Japan Society of Mechanical Engineers, Part C, 2002, 68 (05): : 1435 - 1440
  • [24] Open-loop satellite librational control in elliptic orbits through tether
    Kumar, K
    Kumar, KD
    ACTA ASTRONAUTICA, 1997, 41 (01) : 15 - 21
  • [25] ON ORBIT CONTROL USING GRAVITY GRADIENT EFFECTS
    MURAKAMI, C
    ACTA ASTRONAUTICA, 1981, 8 (07) : 733 - 747
  • [26] Closed form perturbation solution of a fast rotating triaxial satellite under gravity-gradient torque
    M. Lara
    S. Ferrer
    Cosmic Research, 2013, 51 : 289 - 303
  • [27] Frequency analysis of the non-principal-axis rotation of uniaxial space debris in circular orbit subjected to gravity-gradient torque
    Lin, Hou-Yuan
    Zhao, Chang-Yin
    Zhang, Ming-Jiang
    ADVANCES IN SPACE RESEARCH, 2016, 57 (05) : 1189 - 1196
  • [28] Orientation expression and its application to pointing control and utilization of gravity-gradient torque
    Yamada, Katsuhiko
    Yoshikawa, Shoji
    Nippon Kikai Gakkai Ronbunshu, C Hen/Transactions of the Japan Society of Mechanical Engineers, Part C, 2004, 70 (06): : 1770 - 1777
  • [29] Closed form perturbation solution of a fast rotating triaxial satellite under gravity-gradient torque
    Lara, M.
    Ferrer, S.
    COSMIC RESEARCH, 2013, 51 (04) : 289 - 303
  • [30] Control of satellite clusters in elliptic orbit with limited communication
    Chichka, DF
    Belanger, G
    Speyer, JL
    ASTRODYNAMICS, SPACE MISSIONS, AND CHAOS, 2004, 1017 : 177 - 189
12345