Genetik Algoritma Tabanli Kesirli ve Tam Dereceli PID Kontrol Edicilerin Bir Ucąk Modeli Üzerinde Karsilastirilmasi

Gokhan Altintas; Yucel Aydin

Genetik Algoritma Tabanli Kesirli ve Tam Dereceli PID Kontrol Edicilerin Bir Ucąk Modeli Üzerinde Karsilastirilmasi

Gokhan Altintas
, Yucel Aydin

Kontrol ve Otomasyon Mühendisliği Bölümü

Istanbul Technical University

Araştırma çıktısı: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › Hakem

3 Atıf (Scopus)

Özet

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.

Tercüme edilen katkı başlığı	Comparison of fractional and integer order PID controllers on aircraft model using genetic algorithm
Orijinal dil	Türkçe
Ana bilgisayar yayını başlığı	2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016
Yayınlayan	Institute of Electrical and Electronics Engineers Inc.
Sayfalar	242-246
Sayfa sayısı	5
ISBN (Elektronik)	9786050109238
Yayın durumu	Yayınlandı - 10 Şub 2017
Etkinlik	2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016 - Bursa, Türkiye Süre: 1 Ara 2016 → 3 Ara 2016

Yayın serisi

Adı	2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016

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???event.eventtypes.event.conference???	2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016
Ülke/Bölge	Türkiye
Şehir	Bursa
Periyot	1/12/16 → 3/12/16

Bibliyografik not

Publisher Copyright:
© 2016 The Chamber of Turkish Electrical Engineers.

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

Altintas, G., & Aydin, Y. (2017). Genetik Algoritma Tabanli Kesirli ve Tam Dereceli PID Kontrol Edicilerin Bir Ucąk Modeli Üzerinde Karsilastirilmasi. In 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016 (pp. 242-246). Makale 7851882 (2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016). Institute of Electrical and Electronics Engineers Inc..

Altintas, Gokhan ; Aydin, Yucel. / Genetik Algoritma Tabanli Kesirli ve Tam Dereceli PID Kontrol Edicilerin Bir Ucąk Modeli Üzerinde Karsilastirilmasi. 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016. Institute of Electrical and Electronics Engineers Inc., 2017. pp. 242-246 (2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016).

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title = "Genetik Algoritma Tabanli Kesirli ve Tam Dereceli PID Kontrol Edicilerin Bir Uc{\c a}k Modeli {\"U}zerinde Karsilastirilmasi",

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.",

author = "Gokhan Altintas and Yucel Aydin",

note = "Publisher Copyright: {\textcopyright} 2016 The Chamber of Turkish Electrical Engineers.; 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016 ; Conference date: 01-12-2016 Through 03-12-2016",

year = "2017",

month = feb,

day = "10",

language = "T{\"u}rk{\c c}e",

series = "2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

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booktitle = "2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016",

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}

Altintas, G & Aydin, Y 2017, Genetik Algoritma Tabanli Kesirli ve Tam Dereceli PID Kontrol Edicilerin Bir Ucąk Modeli Üzerinde Karsilastirilmasi. in 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016., 7851882, 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016, Institute of Electrical and Electronics Engineers Inc., pp. 242-246, 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016, Bursa, Türkiye, 1/12/16.

Genetik Algoritma Tabanli Kesirli ve Tam Dereceli PID Kontrol Edicilerin Bir Ucąk Modeli Üzerinde Karsilastirilmasi. / Altintas, Gokhan; Aydin, Yucel.
2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016. Institute of Electrical and Electronics Engineers Inc., 2017. p. 242-246 7851882 (2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016).

Araştırma çıktısı: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › Hakem

TY - GEN

T1 - Genetik Algoritma Tabanli Kesirli ve Tam Dereceli PID Kontrol Edicilerin Bir Ucąk Modeli Üzerinde Karsilastirilmasi

AU - Altintas, Gokhan

AU - Aydin, Yucel

PY - 2017/2/10

Y1 - 2017/2/10

N2 - 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.

AB - 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.

UR - https://www.scopus.com/pages/publications/85015371180

M3 - Konferans katkısı

AN - SCOPUS:85015371180

T3 - 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016

SP - 242

EP - 246

BT - 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016

Y2 - 1 December 2016 through 3 December 2016

ER -

Altintas G, Aydin Y. Genetik Algoritma Tabanli Kesirli ve Tam Dereceli PID Kontrol Edicilerin Bir Ucąk Modeli Üzerinde Karsilastirilmasi. In 2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016. Institute of Electrical and Electronics Engineers Inc. 2017. p. 242-246. 7851882. (2016 National Conference on Electrical, Electronics and Biomedical Engineering, ELECO 2016).

Genetik Algoritma Tabanli Kesirli ve Tam Dereceli PID Kontrol Edicilerin Bir Ucąk Modeli Üzerinde Karsilastirilmasi

Özet

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Bibliyografik not

Diğer Dosyalar ve Linkler

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