Detail publikace

Hexacopter Pitch Estimator for a Pitch Stabilizer

BARÁNEK, R. ŠOLC, F.

Originální název

Hexacopter Pitch Estimator for a Pitch Stabilizer

Anglický název

Hexacopter Pitch Estimator for a Pitch Stabilizer

Jazyk

en

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.

Anglický 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.

Dokumenty

BibTex


@inproceedings{BUT102859,
  author="Radek {Baránek} and František {Šolc}",
  title="Hexacopter Pitch Estimator for a Pitch Stabilizer",
  annote="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.",
  address="IFAC-PapersOnLine / Elsevier",
  booktitle="Proceedings of the IFAC/IEEE PDES 2012 International Conference",
  chapter="102859",
  doi="10.3182/20130925-3-CZ-3023.00021",
  howpublished="online",
  institution="IFAC-PapersOnLine / Elsevier",
  year="2013",
  month="september",
  pages="326--329",
  publisher="IFAC-PapersOnLine / Elsevier",
  type="conference paper"
}