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...
Автори: | , |
---|---|
Формат: | Online |
Мова: | spa |
Опубліковано: |
Universidad Pedagógica y Tecnológica de Colombia - UPTC
2015
|
Предмети: | |
Онлайн доступ: | https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/4250 |