Vibration Reduction Design and Test of UAV Load Radar

Table 8

direction simulation and test comparison of model 3.

	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	63.23	60.30	53.53	4.89	4.90	4.97	27.39	38.57	46.15
Test	60.03	56.96	51.57	5.49	5.01	4.30	19.59	28.32	36.97
Error (%)	5.33	5.86	3.80	10.93	2.20	15.58	39.82	36.19	24.83