Result Details

Adaptive Augmentation of an Unmanned Aerial Vehicle's Flight Control System

VLK, J.; CHUDÝ, P. Adaptive Augmentation of an Unmanned Aerial Vehicle's Flight Control System. In Proceedings of 37th Digital Avionics System Conference. London, UK: IEEE Computer Society, 2018. p. 633-641. ISBN: 978-1-5386-4112-5.
Type
conference paper
Language
English
Authors
Vlk Jan, Ing., Ph.D., DCGM (FIT)
Chudý Peter, doc. Ing., Ph.D., MBA, DCGM (FIT)
Abstract

The proposed paper introduces the design of anadaptive augmentation of an Unmanned Aerial Vehicle's (UAV)Flight Control System (FCS). A Linear Quadratic Regulator(LQR) algorithm has been employed as a base-line controlstrategy and enhanced with an adaptation loop based on a ModelReference Adaptive Control (MRAC) technique.

Keywords

adaptive control, aircraft, control hedging, controllaws, dynamic model, flight control system, fixed wing, linearquadratic regulator, Lyapunov stability, model reference adaptivecontrol, simulation, state-space model, unmanned aerial vehicle

Published
2018
Pages
633–641
Proceedings
Proceedings of 37th Digital Avionics System Conference
Conference
37th AIAA/IEEE Digital Avionics Systems Conference
ISBN
978-1-5386-4112-5
Publisher
IEEE Computer Society
Place
London, UK
DOI
10.1109/DASC.2018.8569881
UT WoS
000455217900083
EID Scopus
2-s2.0-85060580812
BibTeX 
@inproceedings{BUT155078,
  author="Jan {Vlk} and Peter {Chudý}",
  title="Adaptive Augmentation of an Unmanned Aerial Vehicle's Flight Control System",
  booktitle="Proceedings of 37th Digital Avionics System Conference",
  year="2018",
  pages="633--641",
  publisher="IEEE Computer Society",
  address="London, UK",
  doi="10.1109/DASC.2018.8569881",
  isbn="978-1-5386-4112-5"
}
Projects
IT4Innovations excellence in science, MŠMT, Národní program udržitelnosti II, LQ1602, start: 2016-01-01, end: 2020-12-31, completed
Departments
Department of Computer Graphics and Multimedia (DCGM)
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