Detail publikace

Hexacopter Pitch Estimator for a Pitch Stabilizer

BARÁNEK, R. ŠOLC, F.

Originální název

Hexacopter Pitch Estimator for a Pitch Stabilizer

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

The paper presents the development and mathematical modelling of an estimator within the control scheme of the pitch motion of a hexacopter. The pitch estimator is constructed as a classic Luenberger-Kalman filter. The authors also discuss the problem of acceleration measurement realized during the flight of the hexacopter. The blade flapping and the related drag are mentioned as the main effects introducing orientation data into the values provided by an accelerometer. A simulation of the designed observer is shown using a simple one-dimensional model.

Klíčová slova

hexacopter, quadrotor, control, flying robot, Luenberger-Kalman observer

Autoři

BARÁNEK, R.; ŠOLC, F.

Rok RIV

2013

Vydáno

25. 9. 2013

Nakladatel

IFAC-PapersOnLine / Elsevier

Místo

IFAC-PapersOnLine 10344 Virginia Lee Dr. Centerville, OH 45458, U.S.A.

ISBN

978-3-902823-21-2

Kniha

Proceedings of the IFAC/IEEE PDES 2012 International Conference

Strany od

326

Strany do

329

Strany počet

4

BibTex

@inproceedings{BUT102859,
  author="Radek {Baránek} and František {Šolc}",
  title="Hexacopter Pitch Estimator for a Pitch Stabilizer",
  booktitle="Proceedings of the IFAC/IEEE PDES 2012 International Conference",
  year="2013",
  pages="326--329",
  publisher="IFAC-PapersOnLine / Elsevier",
  address="IFAC-PapersOnLine
10344 Virginia Lee Dr.
Centerville, OH 45458, U.S.A.",
  doi="10.3182/20130925-3-CZ-3023.00021",
  isbn="978-3-902823-21-2"
}