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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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