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Model based H..control for helicopter vibration reduction - Flight tests with active trailing edge flaps
Model based H..control for helicopter vibration reduction - Flight tests with active trailing edge flaps
2007
O. Dieterich
P. Konstanzer
D. Roth
W. Ayadi
D. Reber
K. H. Well
Keywords:
Aeronautics
Aerospace engineering
Engineering
Vibration
Trailing edge
Structural engineering
h control
Materials science
Correction
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