Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
718858 | IFAC Proceedings Volumes | 2009 | 6 Pages |
Abstract
Sliding mode control synthesis is developed for an underactuated mechanical system. A laboratory helicopter prototype is used as a test bed. Both state feedback design and dynamic output feedback design with sliding mode velocity observers, running in parallel, are proposed. Performance and robustness issues of the closed-loop system are illustrated in a numerical study. The work is in progress and the conference presentation is going to be supported by experimental results.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics