Active Flutter Suppression on an F-4F Aircraft with External Stores Using Already Existing Control Surfaces
Active Flutter Suppression on an F-4F Aircraft with External Stores Using Already Existing Control Surfaces
- New search for: O. Sensburg
- New search for: H. Hoenlinger
- New search for: T. E. Moll
- New search for: O. Sensburg
- New search for: H. Hoenlinger
- New search for: T. E. Moll
The flutter suppression system was flight tested using classical flight flutter tests, open loop tests, and closed loop tests. The control law was found by applying optimal control theory thus minimizing the control surface motion due to disturbances and providing the required stability margins. The selection of the wing mounted store configuration is described.
Document information
Active Flutter Suppression on an F-4F Aircraft with External Stores Using Already Existing Control Surfaces
1980
9 pages
Report
No indication
English
Aircraft , Aerodynamics , Aerodynamic stability , Boundary layer control , Control surfaces , External stores , F-4 aircraft , Feedback control , Flight tests , Flutter , Aerodynamic configurations , Buffeting , Control theory , Flight control , Flutter analysis , Vibrational stress , Wing tanks , Foreign technology
Similar titles
Flutter Analysis of Aircraft with External Stores Using Modal Coupling
| Online Contents | 2004
Flutter Stability of Movable Control Surfaces for Aircraft Stores
| British Library Conference Proceedings | 1999