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
  • [1] Torque Unit Manipulator driven by Control Moment Gyros
    Hokamoto, S
    SPACE COOPERATION INTO THE 21ST CENTURY, 1997, 96 : 865 - 876
  • [2] HIGH-TORQUE CONTROL MOMENT GYROS FOR SPACECRAFT CONTROL
    KIRCHOFF, PW
    SEMINSKI, RB
    SPACE AERONAUTICS, 1967, 47 (05): : 118 - &
  • [3] COMBINED USE OF CONTROL MOMENT GYROS AND MAGNETIC TORQUE RODS FOR SATELLITE ATTITUDE CONTROL
    Elmas, Tuba C.
    Tekinalp, Ozan
    PROCEEDINGS OF THE ASME DYNAMIC SYSTEMS AND CONTROL CONFERENCE 2010, VOL 1, 2010, : 189 - 196
  • [4] CONTROL MOMENT GYROS IN ATTITUDE CONTROL
    JACOT, AD
    LISKA, DJ
    JOURNAL OF SPACECRAFT AND ROCKETS, 1966, 3 (09) : 1313 - &
  • [5] Output torque modeling of control moment gyros considering rolling element bearing induced disturbances
    Wang, Hong
    Han, Qinkai
    Zhou, Daning
    MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2019, 115 : 188 - 212
  • [6] Power Consumption Reduction for Magnetic Bearing Systems During Torque Output of Control Moment Gyros
    Zheng, Shiqiang
    Li, Haitao
    Han, Bangcheng
    Yang, Jingyu
    IEEE TRANSACTIONS ON POWER ELECTRONICS, 2017, 32 (07) : 5752 - 5759
  • [7] Adaptive neural control of spacecraft using control moment gyros
    Leeghim, Henzeh
    Kim, Donghoon
    ADVANCES IN SPACE RESEARCH, 2015, 55 (05) : 1382 - 1393
  • [8] Nonlinear Attitude Control of Drones Using Control Moment Gyros
    Jang, Seok-ho
    Leeghim, Henzeh
    JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2021, 49 (10) : 821 - 828
  • [9] Control method for variable skew configuration control moment gyros
    Zhang Kebei
    Gao Jingmin
    Guan Xin
    Guo Zixi
    CHINESE SPACE SCIENCE AND TECHNOLOGY, 2020, 40 (06) : 23 - 32
  • [10] Attitude control for small satellites using control moment gyros
    Lappas, VJ
    Steyn, WH
    Underwood, CI
    ACTA ASTRONAUTICA, 2002, 51 (1-9) : 101 - 111