Abstract
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.
| Original language | English |
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| Pages | 607-612 |
| Number of pages | 6 |
| Publication status | Published - 1999 |
| Event | Proceedings of the 1999 IEEE International Symposium on Computer Aided Control System Design - Kohala Coat-Island, HI, USA Duration: 22 Aug 1999 → 27 Aug 1999 |
Conference
| Conference | Proceedings of the 1999 IEEE International Symposium on Computer Aided Control System Design |
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| City | Kohala Coat-Island, HI, USA |
| Period | 22/08/99 → 27/08/99 |