Detail výsledku

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.
Typ
článek ve sborníku konference
Jazyk
angličtina
Autoři
Vlk Jan, Ing., Ph.D., UPGM (FIT)
Chudý Peter, doc. Ing., Ph.D., MBA, UPGM (FIT)
Abstrakt

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.

Klíčová slova

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

Rok
2018
Strany
633–641
Sborník
Proceedings of 37th Digital Avionics System Conference
Konference
37th AIAA/IEEE Digital Avionics Systems Conference
ISBN
978-1-5386-4112-5
Vydavatel
IEEE Computer Society
Místo
London, UK
DOI
UT WoS
000455217900083
EID Scopus
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"
}
Projekty
IT4Innovations excellence in science, MŠMT, Národní program udržitelnosti II, LQ1602, zahájení: 2016-01-01, ukončení: 2020-12-31, ukončen
Pracoviště
Nahoru