Flight Test of Pilot-Aircraft Haptic Feedback System

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F19%3APU134739" target="_blank" >RIV/00216305:26210/19:PU134739 - isvavai.cz</a>
Result on the web
<a href="https://www.matec-conferences.org/articles/matecconf/abs/2019/53/matecconf_easn2019_06005/matecconf_easn2019_06005.html" target="_blank" >https://www.matec-conferences.org/articles/matecconf/abs/2019/53/matecconf_easn2019_06005/matecconf_easn2019_06005.html</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1051/matecconf/201930406005" target="_blank" >10.1051/matecconf/201930406005</a>

Result language
angličtina
Original language name
Flight Test of Pilot-Aircraft Haptic Feedback System
Original language description
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.
Czech name
—
Czech description
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Project
<a href="/en/project/TJ01000122" target="_blank" >TJ01000122: Haptic feedback of assistant systems for flight safety improvement</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2019
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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