Fixed gain and adaptive techniques for rotorcraft vibration control
Fixed gain and adaptive techniques for rotorcraft vibration control
- Neue Suche nach: Roy, R. H.
- Neue Suche nach: Saberi, H. A.
- Neue Suche nach: Walker, R. A.
- Neue Suche nach: Roy, R. H.
- Neue Suche nach: Saberi, H. A.
- Neue Suche nach: Walker, R. A.
The results of an analysis effort performed to demonstrate the feasibility of employing approximate dynamical models and frequency shaped cost functional control law desgin techniques for helicopter vibration suppression are presented. Both fixed gain and adaptive control designs based on linear second order dynamical models were implemented in a detailed Rotor Systems Research Aircraft (RSRA) simulation to validate these active vibration suppression control laws. Approximate models of fuselage flexibility were included in the RSRA simulation in order to more accurately characterize the structural dynamics. The results for both the fixed gain and adaptive approaches are promising and provide a foundation for pursuing further validation in more extensive simulation studies and in wind tunnel and/or flight tests.
Dokumentinformationen
Fixed gain and adaptive techniques for rotorcraft vibration control
1985-05-01
Report
Keine Angabe
Englisch
Ähnliche Titel
Adaptive Algorithms for Rotorcraft Active Vibration Control
| British Library Conference Proceedings | 2009