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
| dc.contributor.author | Dieterich, O. | |
| dc.contributor.author | Konstanzer, P. | |
| dc.contributor.author | Roth, D. | |
| dc.contributor.author | Ayadi, W. | |
| dc.contributor.author | Reber, D. | |
| dc.contributor.author | Well, K.H. | |
| dc.date.accessioned | 2016-06-29T15:32:08Z | |
| dc.date.available | 2016-06-29T15:32:08Z | |
| dc.date.issued | 2007 | |
| dc.identifier.uri | http://hdl.handle.net/20.500.11881/199 | |
| dc.language.iso | en | |
| dc.subject.other | Dynamics | |
| dc.title | Model based H..control for helicopter vibration reduction - Flight tests with active trailing edge flaps |
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