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
  • [21] Feedback-based steering law for control moment gyros
    Pechev, Alexandre N.
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2007, 30 (03) : 848 - 855
  • [22] Singularity analysis of variable-speed control moment gyros
    Yoon, H
    Tsiotras, P
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2004, 27 (03) : 374 - 386
  • [23] A NEW STEERING LAW FOR VARIABLE SPEED CONTROL MOMENT GYROS
    Dang, Qingqing
    Jin, Lei
    Xu, Shijie
    SPACEFLIGHT MECHANICS 2017, PTS I - IV, 2017, 160 : 3733 - 3752
  • [24] Volumetric singularity index for a steering law of control moment gyros
    Jin J.
    Jin, Jaehyun (donworry@scnu.ac.kr), 1600, Institute of Control, Robotics and Systems (23): : 8 - 14
  • [25] Steering Law Controlling the Constant Speeds of Control Moment Gyros
    Koyasako, Y.
    Takahashi, M.
    13TH INTERNATIONAL CONFERENCE ON MOTION AND VIBRATION CONTROL (MOVIC 2016) AND THE 12TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN STRUCTURAL DYNAMICS (RASD 2016), 2016, 744
  • [26] Direct Dynamics of a Space Robot Actuated by Control Moment Gyros
    Jia, Yinghong
    Misra, Arun K.
    MACHINES, MECHANISM AND ROBOTICS, 2019, : 123 - 134
  • [27] Singular Direction Escape Steering Law for Control Moment Gyros
    Guo, Yanning
    Cui, Hutao
    Ma, Guangfu
    Li, Chuanjiang
    JOURNAL OF AEROSPACE ENGINEERING, 2017, 30 (05)
  • [28] ON SPACE VEHICLE ATTITUDE STABILIZATION BY PASSIVE CONTROL MOMENT GYROS
    SCHINDEL.JW
    INGENIEUR ARCHIV, 1970, 39 (01): : 37 - &
  • [29] Feasible angular momentum of spacecraft installed with control moment gyros
    Leeghim, Henzeh
    Jin, Jaehyun
    Mok, Sung-Hoon
    ADVANCES IN SPACE RESEARCH, 2018, 61 (01) : 466 - 477
  • [30] PREFERRED GIMBAL ANGLES FOR SINGLE GIMBAL CONTROL MOMENT GYROS
    VADALI, SR
    OH, HS
    WALKER, SR
    AIAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE, PTS 1 AND 2: A COLLECTION OF TECHNICAL PAPERS, 1989, : 443 - 452