Pilot-aircraft haptic feedback tests

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F20%3A00352242" target="_blank" >RIV/68407700:21230/20:00352242 - isvavai.cz</a>

Nalezeny alternativní kódy

RIV/00216305:26210/20:PU136719

Výsledek na webu

<a href="https://doi.org/10.1108/AEAT-12-2019-0265" target="_blank" >https://doi.org/10.1108/AEAT-12-2019-0265</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1108/AEAT-12-2019-0265" target="_blank" >10.1108/AEAT-12-2019-0265</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Pilot-aircraft haptic feedback tests

Popis výsledku v původním jazyce

Purpose - The purpose of this study is to lead to an improvement in pilot-aircraft interaction. The goal of the performed tests is an assessment of haptic feedback, which mediates flight parameters to the pilot. Pedals indicate side-slip angle by vibrations, whereas a sliding element inside the control stick is able to continuously indicate both angles of attack and side-slip. Design/methodology/approach - Haptic feedback applied on rudder pedals and control stick were tested on a flight simulator and flight tests in a couple of tasks. Pilot workload, readability of feedback and side-slip were then evaluated when the flight was turning. Findings - As a useful instrument for aircraft control, haptic feedback was assessed. The feedback settings were then individually perceived, and haptic feedback slightly improved side-slip while turning in a flight test; however, the results are not statistically significant. Practical implications - The tests provided promising results for human pilot performance. The training phase and personal settings of haptic feedback is an approach for improving the performance of human pilots. Originality/value - The designed and tested device is a unique tool for improving pilot-aircraft interaction. This study brings valuable experiences from its flight simulator and in-flight tests.

Název v anglickém jazyce

Pilot-aircraft haptic feedback tests

Popis výsledku anglicky

Purpose - The purpose of this study is to lead to an improvement in pilot-aircraft interaction. The goal of the performed tests is an assessment of haptic feedback, which mediates flight parameters to the pilot. Pedals indicate side-slip angle by vibrations, whereas a sliding element inside the control stick is able to continuously indicate both angles of attack and side-slip. Design/methodology/approach - Haptic feedback applied on rudder pedals and control stick were tested on a flight simulator and flight tests in a couple of tasks. Pilot workload, readability of feedback and side-slip were then evaluated when the flight was turning. Findings - As a useful instrument for aircraft control, haptic feedback was assessed. The feedback settings were then individually perceived, and haptic feedback slightly improved side-slip while turning in a flight test; however, the results are not statistically significant. Practical implications - The tests provided promising results for human pilot performance. The training phase and personal settings of haptic feedback is an approach for improving the performance of human pilots. Originality/value - The designed and tested device is a unique tool for improving pilot-aircraft interaction. This study brings valuable experiences from its flight simulator and in-flight tests.

Druh

J_imp - Článek v periodiku v databázi Web of Science

CEP obor

—

OECD FORD obor

10201 - Computer sciences, information science, bioinformathics (hardware development to be 2.2, social aspect to be 5.8)

Projekt

—

Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2020

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název periodika

Emerald insight

ISSN

1748-8842

e-ISSN

1758-4213

Svazek periodika

92

Číslo periodika v rámci svazku

9

Stát vydavatele periodika

GB - Spojené království Velké Británie a Severního Irska

Počet stran výsledku

6

Strana od-do

1407-1412

Kód UT WoS článku

000525575500001

EID výsledku v databázi Scopus

2-s2.0-85083375305