Copy For Citation
ERMEYDAN A., KIYAK E.
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, vol.89, no.3, pp.468-476, 2017 (SCI-Expanded)
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Publication Type:
Article / Article
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Volume:
89
Issue:
3
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Publication Date:
2017
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Doi Number:
10.1108/aeat-04-2015-0096
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Journal Name:
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
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Journal Indexes:
Science Citation Index Expanded (SCI-EXPANDED), Scopus
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Page Numbers:
pp.468-476
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Keywords:
Quadrotor, Enhanced PID controller, Fault tolerant control, Nonlinear model, PREDICTIVE CONTROL, CONTROL-SYSTEM, QUAD-ROTOR, DESIGN
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Anadolu University Affiliated:
Yes
Abstract
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.