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Alleviation of tiltrotor wing-root vibratory loads through cyclic control approach
Colella, M. Molica
;
Bernardini, G.
;
Gennaretti, M.
(
2009
)
Model based H..control for helicopter vibration reduction - Flight tests with active trailing edge flaps
Dieterich, O.
;
Konstanzer, P.
;
Roth, D.
;
Ayadi, W.
;
Reber, D.
;
Well, K.H.
(
2007
)
Experimental investigation of an active twist model rotor blade under centrifugal loads
Wierach, P.
;
Riemenschneider, J.
;
Optiz, S.
;
Hoffmann, F.
(
2007
)
Active cabin vibration reduction for jet-smooth helicopter ride
Hoffmann, F.
;
Konstanzer, M.
;
Priems, M.
;
Chemin, J.
(
2009
)
Using multibody dynamics for the simulation of flexible rotor blades - getting the mechanical coupling right?
Arnold, J.
(
2009
)
Achieving simultaneous reduction of rotorcraft vibration and noise using simulation
Patt, D.
;
Liu, L.
;
Friedmann, P.P.
(
2004
)
Measuring blade angular motions: A kinematical approach
Attilio, C.
;
Locatelli, A.
(
2004
)
Modelling design prototyping of control laws for the Bell-412 advanced systems research aircraft
Walker, D.J.
;
Manimala, B.J.
;
Voskuijl, M.
;
Gubbels, A.W.
(
2007
)
Review of the common DLR/ONERA project "Active twist blade"(ATB)
Riemenschneider, J.
;
Keye, S.
;
Wierach, P.
;
Mercier des Rochettes, H.
(
2004
)
Cloosed loop IBC results from recent CH-53G flight tests
Arnold, U.T.P.
;
Fürst, D.
(
2004
)
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Gennaretti, M. (6)
Ghiringhelli, G.L. (5)
Masarati, P. (5)
Nitzsche, F. (4)
Bernardini, G. (3)
Chopra, I. (3)
Dieterich, O. (3)
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Serafini, J. (3)
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