Robust output tracking control of an unmanned aerial vehicle subject to additive state dependent disturbance-Reference-Cited by-同舟云学术

Robust output tracking control of an unmanned aerial vehicle subject to additive state dependent disturbance

Published:2016-07-14 Issue:14 Volume:10 Page:1612-1619
ISSN:1751-8652
Container-title:IET Control Theory & Applications
language:en
Short-container-title:IET Control Theory & Applications

Author:

Tanyer İlker¹,Tatlıcıoğlu Enver¹,Zergeroğlu Erkan²,Deniz Meryem¹,Bayrak Alper³,Özdemirel Barbaros¹

Affiliation:

1. Department of Electrical & Electronics Engineeringİzmir Institute of TechnologyUrlaİzmir35430Turkey

2. Department of Computer EngineeringGebze Technical UniversityGebzeKocaeli41400Turkey

3. Department of Electrical & Electronics EngineeringAbant İzzet Baysal UniversityBolu14280Turkey

Publisher

Institution of Engineering and Technology (IET)

Subject

Electrical and Electronic Engineering,Control and Optimization,Computer Science Applications,Human-Computer Interaction,Control and Systems Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1049/iet-cta.2015.1304

Reference30 articles.

1. Dynamic inversion: an evolving methodology for flight control design

2. Robust flight control design using dynamic inversion and structured singular value synthesis

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