Torque amplification of control moment gyros

被引:40
|
作者
Lappas, VJ [1 ]
Steyn, WH [1 ]
Underwood, CI [1 ]
机构
[1] Univ Surrey, Surrey Space Ctr, Guildford GU2 5XH, Surrey, England
关键词
Attitude control systems - Single gimbal control moment gyro;
D O I
10.1049/el:20020590
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Control moment gyros (CMG) are considered to be powerful actuators for satellites due to their large potential torque capability (torque amplification). A way to optimise the torque amplification generated by CMGs via an incremental manoeuvre control strategy is presented.
引用
收藏
页码:837 / 839
页数:3
相关论文
共 50 条
  • [41] Nonlinear Attitude Control of Flexible Spacecraft With Scissored Pairs of Control Moment Gyros
    Fan, Jixiang
    Zhou, Di
    JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 2012, 134 (05):
  • [42] Maneuver control of the hypersonic gliding vehicle with a scissored pair of control moment gyros
    Kun Zhao
    DengQing Cao
    WenHu Huang
    Science China Technological Sciences, 2018, 61 : 1150 - 1160
  • [43] Retrospective Cost Adaptive Spacecraft Attitude Control using Control Moment Gyros
    Camblor, Marc
    Cruz, Gerardo
    Esteban, Sergio
    Leve, Fred A.
    Bernstein, Dennis S.
    2014 AMERICAN CONTROL CONFERENCE (ACC), 2014, : 2492 - 2497
  • [44] Maneuver control of the hypersonic gliding vehicle with a scissored pair of control moment gyros
    ZHAO Kun
    CAO DengQing
    HUANG WenHu
    Science China(Technological Sciences), 2018, (08) : 1150 - 1160
  • [45] Feedback Control with Nominal Inputs for Agile Satellites Using Control Moment Gyros
    Kusuda, Y.
    Takahashi, M.
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2011, 34 (04) : 1209 - 1218
  • [46] Modified Singular-Direction Avoidance Steering for Control Moment Gyros
    Meng, Tao
    Matunaga, Saburo
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2011, 34 (06) : 1915 - 1920
  • [47] OPTIMAL CONFIGURATION OF CONTROL MOMENT GYROS FOR MINIMUM ENERGY MANEUVERS OF SATELLITES
    Uematsu, Eijiro
    Ueno, Seiya
    Higuchi, Takehiro
    SPACE FOR OUR FUTURE, 2013, 146 : 41 - 55
  • [48] MAGNETIC TORQUERS FOR MOMENTUM DESATURATION OF SPACE STATION CONTROL MOMENT GYROS
    BUCKINGHAM, AG
    BRAUMILLER, J
    JOURNAL OF SPACECRAFT AND ROCKETS, 1972, 9 (06) : 387 - +
  • [49] Steering law for parallel mounted double gimbaled control moment gyros
    School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
    不详
    Yuhang Xuebao, 2009, 4 (1551-1556+1563): : 1551 - 1556
  • [50] Internal disturbance accommodation filter of control moment gyros with adaptive observer
    Takahashi, Masaki
    Shimizu, Sefichi
    Taniwaki, Shigemune
    Yoshida, Kazuo
    Ohkami, Yoshiaki
    ASTRODYNAMICS 2007, PTS I-III, 2008, 129 : 1397 - 1411