DocumentCode :
490267
Title :
VHHC in Helicopters
Author :
Kabamba, P.T. ; Meerkov, S.M. ; Poh, E.-K.
Author_Institution :
Department of Aerospace Engineering, The University of Michigan, Ann Arbor, MI 48109-2140
fYear :
1993
fDate :
2-4 June 1993
Firstpage :
1118
Lastpage :
1122
Abstract :
Higher Harmonic Control (HHC) is a method for cancelling the helicopter fuselage vibrations by introducing N/rev oscillations of rotor blades pitch angle (N is the number of rotor blades). This method is effective if both the amplitude and the phase of the oscillations introduced are chosen appropriately, depending on the flight conditions. It is shown in this paper that if the frequency of these oscillations is much greater than N/rev, the phase dependency disappears.
Keywords :
Aerodynamics; Blades; Frequency; Helicopters; Military aircraft; Open loop systems; Rotors; Vehicle dynamics; Vibration control; Vibration measurement;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1993
Conference_Location :
San Francisco, CA, USA
Print_ISBN :
0-7803-0860-3
Type :
conf
Filename :
4793040
Link To Document :
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