Abstract
In this study, a model related between pitch angle and elevator deflection angle of an aircraft is derived. Based on this model integer order and fractional order PID controller is designed. Genetic algorithm is used as optimization method to determine the controller parameters. Fitness function is evaluated during the optimization process to find controller coefficients to minimize. Controllers are tested in steady and variable reference input condition and their performance index are compared. Also fractional parameters variation effects are analyzed.
Translated title of the contribution | Comparison of fractional and integer order PID controllers on aircraft model using genetic algorithm |
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Original language | Turkish |
Title of host publication | 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016 |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 242-246 |
Number of pages | 5 |
ISBN (Electronic) | 9786050109238 |
Publication status | Published - 10 Feb 2017 |
Event | 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016 - Bursa, Turkey Duration: 1 Dec 2016 → 3 Dec 2016 |
Publication series
Name | 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016 |
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Conference
Conference | 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016 |
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Country/Territory | Turkey |
City | Bursa |
Period | 1/12/16 → 3/12/16 |
Bibliographical note
Publisher Copyright:© 2016 The Chamber of Turkish Electrical Engineers.