Robust Controller LMI for helicopter with two degrees of freedom
This article presents the design of a robust H∞ controller using techniques of linear matrix inequalities (LMIs) for controlling the position of Pitch and Yaw in a helicopter. Designing a FF + LMI controller is presented for stabilizing the system, and further the design of LMI + FF + integrator con...
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| Format: | Online |
| Sprache: | spa |
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Universidad Pedagógica y Tecnológica de Colombia - UPTC
2015
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| Online Zugang: | https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/4250 |
