Vibration Reduction Design and Test of UAV Load Radar

Table 6

direction simulation and test comparison of model 1.

	First order peak frequency (Hz)			Peak magnification			100 Hz amplitude reduction effect
	0.2 g	0.5 g	1.0 g	0.2 g	0.5 g	1.0 g	0.2 g	0.5 g	1.0 g
Simulation	70.07	70.06	70.00	3.89	3.87	3.92	7.92	7.96	7.90
Test	60.03	56.96	51.57	5.49	5.01	4.30	19.59	28.32	36.97
Error (%)	16.72	23.00	35.74	29.14	22.75	8.84	59.57	71.89	78.63