Abstract
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.
Original language | English |
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Pages (from-to) | 37-43 |
Number of pages | 7 |
Journal | Journal of Aeronautics, Astronautics and Aviation |
Volume | 43 |
Issue number | 1 |
Publication status | Published - 2011 Mar |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Space and Planetary Science