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.