Adaptive strategies for the active control of helicopter vibration
Helicopter fuselage vibrations are of significant levels and produce a unique vibration problem. Reducing the vibration levels increases passenger comfort, reduces crew fatigue, allows higher cruise speeds to be achieved and improves equipment reliability. Vibration Reduction Techniques can be divid...
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Main Author: | John T. Pearson |
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Format: | Default Thesis |
Published: |
1994
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Subjects: | |
Online Access: | https://hdl.handle.net/2134/11074 |
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