Research on Microvibrations Generated by a Control Moment Gyroscope on a Flexible Interface Based on a Dynamic Substructure Method

Table 5

Mean values of disturbance amplitude on two interfaces.

Component	Flexible interface	Rigid interface	Ratio
Fx	3.99 N	2.89 N	1.38
Fy	5.84 N	2.45 N	2.38
Fz	0.64 N	2.54 N	0.25
Mx	0.57 N·m	0.15 N·m	3.81
My	0.31 N·m	0.18 N·m	1.72
Mz	0.03 N·m	0.01 N·m	2.11