Özet
In this paper a new variable structure control law for uncertain MIMO systems is investigated. The conditions for the existence of a sliding mode is derived. The asymptotic stability in large of the VSS is studied by using Lyapunov V-function method. By these conditions successfully designed the longitudinal position and tracking variable structure control systems for the F-18 aircraft MIMO model with parameter perturbations. Longitudinal dynamics of F-18 aircraft with parameter perturbations is considered. Finally simulation results for VSS with chattering and free of chattering cases are presented to show the effectiveness of the design methods.
| Orijinal dil | İngilizce |
|---|---|
| Sayfalar | 607-612 |
| Sayfa sayısı | 6 |
| Yayın durumu | Yayınlandı - 1999 |
| Etkinlik | Proceedings of the 1999 IEEE International Symposium on Computer Aided Control System Design - Kohala Coat-Island, HI, USA Süre: 22 Ağu 1999 → 27 Ağu 1999 |
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| ???event.eventtypes.event.conference??? | Proceedings of the 1999 IEEE International Symposium on Computer Aided Control System Design |
|---|---|
| Şehir | Kohala Coat-Island, HI, USA |
| Periyot | 22/08/99 → 27/08/99 |
Parmak izi
Design of longitudinal variable structure flight control system for the F-18 aircraft model with parameter perturbations' araştırma başlıklarına git. Birlikte benzersiz bir parmak izi oluştururlar.Alıntı Yap
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