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Semi-active vibration control for wing aileron using stepped magneto-rheological damper
Wei Sun
*
,
Haiyan Hu
*
Corresponding author for this work
Nanjing University of Aeronautics and Astronautics
Research output
:
Contribution to journal
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Article
›
peer-review
3
Citations (Scopus)
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Engineering
Optimal Control
100%
Active Vibration Control
100%
Computer Simulation
50%
Magnetic Field
50%
Illustrates
50%
Control Strategy
50%
Active Control
50%
Specifies
50%
Critical Flutter Speed
50%
Rotation Axis
50%