Detail publikace

Flight Test of Pilot-Aircraft Haptic Feedback System

ZIKMUND, P. DUBNICKÝ, L. HORPATZKÁ, M. MACÍK, M. JEBÁČEK, I.

Anglický název

Flight Test of Pilot-Aircraft Haptic Feedback System

Typ

Stať ve sborníku v databázi WoS či Scopus

Jazyk

en

Originální abstrakt

This research is focused on an innovative improvement of pilot-aircraft interaction and is targeted on small aircraft. Haptic feedback is performed by actuators mounted on an aircraft's controls. The purpose of the actuators on a control stick and pedals is stall warning and a pilot guiding to safe and economical flight regimes. The feedback system mediates airflow data as angles of attack and sideslip. The paper brings results of a flight test of the proposed system. Qualitative evaluation of the haptic feedback inflight is presented. Benefits of the system are presented on a sideslip during turning. Some recommendations for the haptic pilot-aircraft interaction are stated within the discussion of the flight test results.

Klíčová slova anglicky

Flight test, Haptic feedback; Pilot-aircraft interaction

Vydáno

2019-12-17

Nakladatel

MATEC Web of Conferences

ISSN

2261-236X

Kniha

MATEC Web of Conferences

Časopis

MATEC web of conferences

Ročník

2019

Číslo

304

Strany od–do

1–7

Počet stran

7

BIBTEX


@inproceedings{BUT161156,
  author="Pavel {Zikmund} and Lukáš {Dubnický} and Michaela {Horpatzká} and Miroslav {Macík} and Ivo {Jebáček}",
  title="Flight Test of Pilot-Aircraft Haptic Feedback System",
  booktitle="MATEC Web of Conferences",
  year="2019",
  series="9th EASN International Conference on “Innovation in Aviation & Space”",
  journal="MATEC web of conferences",
  volume="2019",
  number="304",
  pages="1--7",
  publisher="MATEC Web of Conferences",
  doi="10.1051/matecconf/201930406005",
  issn="2274-7214",
  url="https://www.matec-conferences.org/articles/matecconf/abs/2019/53/matecconf_easn2019_06005/matecconf_easn2019_06005.html"
}