摘要
This work obtains the appropriate parameters for proportional, integral, and derivative controllers for a Twin Rotor Multivariable System to achieve good tracking performance using a novel method combined with the model reduction method. The Fuzzy control method with the multi-section gains and derivatives is also applied to improve tracking performance and solve the disturbance problem caused by the air flows. Both methods are implemented by the proposed real-time control system. Simulation and experiment results verify the effectiveness of the proposed methods.
原文 | English |
---|---|
頁(從 - 到) | 37-43 |
頁數 | 7 |
期刊 | Journal of Aeronautics, Astronautics and Aviation |
卷 | 43 |
發行號 | 1 |
出版狀態 | Published - 2011 三月 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Space and Planetary Science