A Novel Vibration Control System Applying Annularly Arranged Thrusters for Multiple Launch Rocket System in Launching Process

Table 2

Comparison of in the control period under Condition 2.

The rocket order	Without control	With control under Condition 1	Reduction percentage (%)
1	0.0038	0.0038	0
2	0.0143	0.0099	30.35
3	0.0136	0.0094	30.66
4	0.0161	0.0101	37.29
5	0.0143	0.0098	31.55
6	0.0206	0.0138	33.14
7	0.0192	0.0121	37.17
8	0.0165	0.0088	46.43
9	0.0257	0.0117	54.96
10	0.0181	0.0140	22.79
11	0.0243	0.0161	33.74
12	0.0165	0.0117	29.45
13	0.0194	0.0181	6.70
14	0.0155	0.0091	40.87
15	0.0182	0.0148	18.56
16	0.0269	0.0167	37.77
17	0.0220	0.0132	40.28
18	0.0126	0.0096	23.23
The average value	0.01765	0.0121	31.43