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https://doi.org/10.1109/CCA.2007.4389241
| Title: | Output trajectory tracking for a switched nonlinear non-minimum phase system: The VSTOL aircraft | Authors: | Benosman, M. Lum, K.Y. |
Issue Date: | 2007 | Citation: | Benosman, M.,Lum, K.Y. (2007). Output trajectory tracking for a switched nonlinear non-minimum phase system: The VSTOL aircraft. Proceedings of the IEEE International Conference on Control Applications : 262-269. ScholarBank@NUS Repository. https://doi.org/10.1109/CCA.2007.4389241 | Abstract: | This work concerns output trajectory tracking for the McDonnell Dougglas YAV68B Harrier VSTOL aircraft. This system can perform three distinct flight modes, and is modelled with a Lagrangian nonlinear hybrid non-minimum phase dynamics. Output tracking is solved using classical input/output linearization scheme associated to an internal dynamics stable inversion for each flight mode dynamics. The performance of the global switched control law is discussed and validated through simulation tests. © 2007 IEEE. | Source Title: | Proceedings of the IEEE International Conference on Control Applications | URI: | http://scholarbank.nus.edu.sg/handle/10635/111625 | ISBN: | 1424404436 | DOI: | 10.1109/CCA.2007.4389241 |
| Appears in Collections: | Staff Publications |
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