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 4 条
  • [1] [Anonymous], 1998, AIAA ED SERIES
  • [2] BEDROSSIAN NS, 1987, THESIS MIT
  • [3] LAPPAS VJ, 2001, ELECT LETT, V37
  • [4] WIE B, 2000, AIAA GUID NAV CONTR