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

Table 1

Comparison of in the control period under Condition 1.

The rocket order	Without control	With control under Condition 1	Reduction percentage (%)
1	0.0038	0.0022	41.47
2	0.0143	0.0105	26.20
3	0.0136	0.0108	20.24
4	0.0161	0.0139	13.62
5	0.0143	0.0105	26.50
6	0.0206	0.0160	22.27
7	0.0192	0.0151	21.64
8	0.0165	0.0166	-0.58
9	0.0257	0.0209	18.71
10	0.0181	0.0163	9.86
11	0.0243	0.0197	19.22
12	0.0165	0.0148	10.27
13	0.0194	0.0192	0.82
14	0.0155	0.0122	20.78
15	0.0182	0.0145	20.12
16	0.0269	0.0185	31.45
17	0.0220	0.0159	27.87
18	0.0126	0.0085	32.40
The average value	0.1765	0.01424	19.32