| Translated title of the contribution | Use of bifurcation and continuation methods in the identification and control of aeroelastic induced effects on flexible aircraft dynamics |
|---|---|
| Original language | English |
| Title of host publication | 51st AIAA/ASEM/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference |
| Publication status | Published - Apr 2010 |
Bibliographical note
Name and Venue of Event: 18th AIAA/ASME/AHS Adaptive Structures Conference, Orlando, USAConference Organiser: AIAA