Atıf İçin Kopyala
ERMEYDAN A., KIYAK E.
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.89, sa.3, ss.468-476, 2017 (SCI-Expanded)
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Yayın Türü:
Makale / Tam Makale
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Cilt numarası:
89
Sayı:
3
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Basım Tarihi:
2017
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Doi Numarası:
10.1108/aeat-04-2015-0096
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Dergi Adı:
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
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Derginin Tarandığı İndeksler:
Science Citation Index Expanded (SCI-EXPANDED), Scopus
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Sayfa Sayıları:
ss.468-476
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Anahtar Kelimeler:
Quadrotor, Enhanced PID controller, Fault tolerant control, Nonlinear model, PREDICTIVE CONTROL, CONTROL-SYSTEM, QUAD-ROTOR, DESIGN
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Anadolu Üniversitesi Adresli:
Evet
Özet
Purpose - The purpose of this paper is to present fault tolerant control of a quadrotor based on the enhanced proportional integral derivative (PID) structure in the presence of one or more actuator faults.