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...
- Autores:
- Tipo de recurso:
- http://purl.org/coar/resource_type/c_6519
- Fecha de publicación:
- 2015
- Institución:
- Universidad Pedagógica y Tecnológica de Colombia
- Repositorio:
- RiUPTC: Repositorio Institucional UPTC
- Idioma:
- spa
- OAI Identifier:
- oai:repositorio.uptc.edu.co:001/12252
- Acceso en línea:
- https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/4250
https://repositorio.uptc.edu.co/handle/001/12252
- Palabra clave:
- robust control
linear matrix inequalities
nominal model
nonlinear systems.
control robusto
desigualdades matriciales lineales
modelo nominal
sistema no lineal
- Rights
- License
- Derechos de autor 2015 Ingeniería Investigación y Desarrollo
| Summary: | 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 controller is performed to make the tracking error equal to zero. Thereafter the results of simulations are showed on the nonlinear system model and a comparison with FF+LQR and FF+LQR+I which were developed by device manufacturers. |
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