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 are illustrated in a numerical study.
Original language | English |
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Article number | 6163529 |
Pages (from-to) | 361-366 |
Number of pages | 6 |
Journal | Proceedings of IEEE International Workshop on Variable Structure Systems |
DOIs | |
State | Published - 2012 |
Event | 2012 12th International Workshop on Variable Structure Systems, VSS 2012 - Mumbai, India Duration: 12 Jan 2012 → 14 Jan 2012 |