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...
| প্রধান লেখক: | , |
|---|---|
| বিন্যাস: | Online |
| ভাষা: | spa |
| প্রকাশিত: |
Universidad Pedagógica y Tecnológica de Colombia - UPTC
2015
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| বিষয়গুলি: | |
| অনলাইন ব্যবহার করুন: | https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/4250 |
