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Shock and Vibration
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Shock and Vibration
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2018
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Article
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Tab 1
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Research Article
An Aerodynamic Load Correction Method for HFFB Technique Based on Signal Decoupling and an Intelligent Optimization Algorithm
Table 1
Parameter settings for signal simulation.
Case number
Signal
Function
Frequency
Sample size
Noise level
1
S1
S2
0.010
0.015
200
-
2
S1
S2
0.020
0.025
200
-
3
S1
S2
S3
0.025
0.030
0
200
-30