Conference
Open access
Aug 2026
Research on an indirectly driven servo system for CMG frameworks based on dual-angle-sensor technology
As the core actuator for spacecraft attitude control, the precision of the control moment gyroscope (CMG) frame servo system directly affects the attitude stability of the spacecraft. Addressing the performance degradation caused by nonlinear factors—such as flexibility, transmission errors, and backlash—introduced by...
Yue-Wei Hu, Zhu-Lin Liang, Ming Lu et al.
· Journal of Physics, Conferen... · 0 citations