Design of LMI+I controller based in optimization for two degree of Freedom Helicopter
Its presents the Genetic Algorithms' use for the design's optimization of a Robust control H8 using lineal Matrix Inequalities' techniques, to control pitch and yaw's position in a two degrees of freedom helicopter. The optimization is carried out when the pitch and yaw'...
- Autores:
- Tipo de recurso:
- http://purl.org/coar/resource_type/c_6686
- Fecha de publicación:
- 2007
- Institución:
- Universidad Pedagógica y Tecnológica de Colombia
- Repositorio:
- RiUPTC: Repositorio Institucional UPTC
- Idioma:
- spa
- OAI Identifier:
- oai:repositorio.uptc.edu.co:001/12133
- Acceso en línea:
- https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856
https://repositorio.uptc.edu.co/handle/001/12133
- Palabra clave:
- optimization
robust control
linear matrix inequatilities
helicopter
genetic algorithms
optimización
control robusto
desigualdades matriciales lineales
helicóptero
algoritmos genéticos
- Rights
- License
- Derechos de autor 2007 Ingeniería Investigación y Desarrollo
| Summary: | Its presents the Genetic Algorithms' use for the design's optimization of a Robust control H8 using lineal Matrix Inequalities' techniques, to control pitch and yaw's position in a two degrees of freedom helicopter. The optimization is carried out when the pitch and yaw's speed sensor, based on the energy consumption fails, the maximum peak and oscillation frequency of the system. The simulations' results are presented on the non-linear model system. |
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