Detail publikace

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

VLK, J. CHUDÝ, P.

Originální název

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

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

The proposed paper introduces the design of an adaptive 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 control strategy and enhanced with an adaptation loop based on a Model Reference Adaptive Control (MRAC) technique.

Klíčová slova

adaptive control, aircraft, control hedging, control laws, dynamic model, flight control system, fixed wing, linear quadratic regulator, Lyapunov stability, model reference adaptive control, simulation, state-space model, unmanned aerial vehicle

Autoři

VLK, J.; CHUDÝ, P.

Vydáno

23. 9. 2018

Nakladatel

IEEE Computer Society

Místo

London, UK

ISBN

978-1-5386-4112-5

Kniha

Proceedings of 37th Digital Avionics System Conference

Strany od

633

Strany do

641

Strany počet

9

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"
}