Abstract
The possibility of using a laser sensor and piezoelectric patches for vibration suppression on aircraft was demonstrated. The control technique significantly increased the damping ratio and reduced the steady-state vibration of a model wing in a low-speed wind tunnel. The performance could be improved by using actuators that have a large force and a filter with less phase lag. It was shown that the laser can operate in clouds, and darkness has no effect on laser.
| Original language | English |
|---|---|
| Pages (from-to) | 1394-1398 |
| Number of pages | 5 |
| Journal | AIAA journal |
| Volume | 43 |
| Issue number | 6 |
| DOIs | |
| State | Published - Jan 1 2005 |
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