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

Table 6

Simulation error of the dynamic response on the DSM (%).

Gimbal angle	TAx	TAy	TAz	AAx	AAy	AAz
0°	−4.44	−3.47	−3.31	−3.15	−4.48	−3.47
30°	−3.96	−3.63	−2.23	−3.47	−3.84	−3.91
60°	−2.96	−4.08	−1.25	−4.21	−2.64	−4.51
90°	−2.11	−4.37	−0.81	−4.74	−1.08	−4.69
120°	−2.75	−3.84	−1.12	−4.20	−4.23	−3.80
150°	−3.73	−3.21	−2.17	−3.45	−4.69	−3.10
180°	−4.50	−2.93	−4.01	−3.02	−5.15	−2.94
210°	−4.01	−3.19	−2.09	−3.42	−4.35	−3.30
240°	−2.91	−3.88	−1.20	−4.31	−2.79	−3.82
270°	−1.87	−4.37	−0.80	−4.76	−0.83	−3.74
300°	−2.84	−4.03	−1.12	−4.06	−4.09	−2.98
330°	−3.69	−3.64	−2.11	−3.40	−3.90	−3.16
360°	−4.44	−3.47	−3.31	−3.16	−4.49	−3.47