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
Aircraft , Vibration , Helicopters , Control , Absorbers(Equipment) , Dynamic response , Resonant frequency , Helicopter rotors , Mathematical models , Excitation , Structural response , Aircraft equipment , Frequency response , Numerical analysis , Dynamic vibration absorbers , Antiresonance , Active control
Helicopter flight vibration problems
Engineering Index Backfile | 1955
|HELICOPTER MANEUVER PERFORMANCE WITH ACTIVE LOAD LIMITING
TIBKAT | 2020
|Chaos in nonlinear dynamic systems: helicopter vibration mechanisms
Tema Archiv | 2007
|