Model based H..control for helicopter vibration reduction - Flight tests with active trailing edge flaps

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dc.contributor.authorDieterich, O.
dc.contributor.authorKonstanzer, P.
dc.contributor.authorRoth, D.
dc.contributor.authorAyadi, W.
dc.contributor.authorReber, D.
dc.contributor.authorWell, K.H.
dc.date.accessioned2016-06-29T15:32:08Z
dc.date.available2016-06-29T15:32:08Z
dc.date.issued2007
dc.identifier.urihttp://hdl.handle.net/20.500.11881/199
dc.language.isoen
dc.subject.otherDynamics
dc.titleModel based H..control for helicopter vibration reduction - Flight tests with active trailing edge flaps

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