This report summarizes the accomplishments of a study exploring new methods for the vibration control of helicopters. Reanalysis methodology permits a variety of vibration control problems to be solved efficiently. Both analytical and experimental studies have been conducted. (Author)
Limiting Performance of Nonlinear Systems with Applications to Helicopter Vibration Control Problems
1982
26 pages
Report
Keine Angabe
Englisch
Helicopter rotors , Mathematical models , Vibration , Aircraft equipment , Excitation , Control , Aircraft , Absorbers(Equipment) , Dynamic vibration absorbers , Frequency response , Antiresonance , Dynamic response , Structural response , Numerical analysis , Helicopters , Resonant frequency , Active control
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