HHO Algorithm based PID Controller Design for Aircraft Pitch Angle Control System

Davut Izci, Serdar Ekinci, Aysen Demiroren, John Hedley

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde BölümKonferans katkısıbilirkişi

39 Atıf (Scopus)

Özet

In this study, Harris hawks optimization (HHO) algorithm has been proposed as a novel meta-heuristic algorithm to achieve optimal parameters of a PID controller adopted for aircraft pitch control system. To evaluate the performance of the proposed approach, comparative analyses have been performed using statistical analysis along with time and frequency domain analyses. Other recent and effective meta-heuristic algorithms based PID controllers such as salp swarm algorithm (SSA) tuned and atom search optimization (ASO) algorithm tuned PID controllers were chosen for comparison to verify the effectiveness of HHO tuned PID controller. The comparisons have confirmed the better performance of the proposed HHO tuned PID controller over other mechanisms for controlling the pitch angle of an aircraft.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığıHORA 2020 - 2nd International Congress on Human-Computer Interaction, Optimization and Robotic Applications, Proceedings
YayınlayanInstitute of Electrical and Electronics Engineers Inc.
ISBN (Elektronik)9781728193526
DOI'lar
Yayın durumuYayınlandı - Haz 2020
Etkinlik2nd International Congress on Human-Computer Interaction, Optimization and Robotic Applications, HORA 2020 - Ankara, Turkey
Süre: 26 Haz 202027 Haz 2020

Yayın serisi

AdıHORA 2020 - 2nd International Congress on Human-Computer Interaction, Optimization and Robotic Applications, Proceedings

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???event.eventtypes.event.conference???2nd International Congress on Human-Computer Interaction, Optimization and Robotic Applications, HORA 2020
Ülke/BölgeTurkey
ŞehirAnkara
Periyot26/06/2027/06/20

Bibliyografik not

Publisher Copyright:
© 2020 IEEE.

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