The detection of pilot‐induced oscillations

Fly‐by‐wire systems enable superior control of chosen flight parameters. A pilot can modify stabilized parameters by adequate movement of control inceptors such as a side‐stick or trust lever. Fly‐by‐wire control reduces the load on a pilot and allows a pilot to focus on the main tasks. Unfortunatel...

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Main Author: Paweł Rzucidło
Format: Article
Language:English
Published: Vilnius Gediminas Technical University 2007-03-01
Series:Aviation
Subjects:
Online Access:https://bjrbe.vgtu.lt/index.php/Aviation/article/view/7018
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author Paweł Rzucidło
author_facet Paweł Rzucidło
author_sort Paweł Rzucidło
collection DOAJ
description Fly‐by‐wire systems enable superior control of chosen flight parameters. A pilot can modify stabilized parameters by adequate movement of control inceptors such as a side‐stick or trust lever. Fly‐by‐wire control reduces the load on a pilot and allows a pilot to focus on the main tasks. Unfortunately, the use of more complicated interfaces between human and machine can cause incorrect pilot behavior and in many cases lead to erroneous interactions between the operator and effective aircraft dynamics. The structure of control laws and dynamics of electromechanical actuators are especially important factors. They can influence unfavorable aircraft‐pilot coupling and can lead to pilot‐induced oscillations (PIO) in certain cases. The automatic detection of PIOs is presented in this paper. The practical realization of a PIO‐detector and examples of diagnostics of human‐machine systems are reported on in this article. First published online: 14 Oct 2010
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spelling doaj.art-adedb9a5533e449d9fa1b58aad4b3eb02022-12-21T20:20:49ZengVilnius Gediminas Technical UniversityAviation1648-77881822-41802007-03-0111110.3846/16487788.2007.9635950The detection of pilot‐induced oscillationsPaweł Rzucidło0Rzeszów University of Technology, Department of Avionics and Control, ul. W. Pola 2, 35-959 Rzeszów, PolandFly‐by‐wire systems enable superior control of chosen flight parameters. A pilot can modify stabilized parameters by adequate movement of control inceptors such as a side‐stick or trust lever. Fly‐by‐wire control reduces the load on a pilot and allows a pilot to focus on the main tasks. Unfortunately, the use of more complicated interfaces between human and machine can cause incorrect pilot behavior and in many cases lead to erroneous interactions between the operator and effective aircraft dynamics. The structure of control laws and dynamics of electromechanical actuators are especially important factors. They can influence unfavorable aircraft‐pilot coupling and can lead to pilot‐induced oscillations (PIO) in certain cases. The automatic detection of PIOs is presented in this paper. The practical realization of a PIO‐detector and examples of diagnostics of human‐machine systems are reported on in this article. First published online: 14 Oct 2010https://bjrbe.vgtu.lt/index.php/Aviation/article/view/7018pilot‐induced oscillationsPIOdetectorfly‐by‐wire
spellingShingle Paweł Rzucidło
The detection of pilot‐induced oscillations
Aviation
pilot‐induced oscillations
PIO
detector
fly‐by‐wire
title The detection of pilot‐induced oscillations
title_full The detection of pilot‐induced oscillations
title_fullStr The detection of pilot‐induced oscillations
title_full_unstemmed The detection of pilot‐induced oscillations
title_short The detection of pilot‐induced oscillations
title_sort detection of pilot induced oscillations
topic pilot‐induced oscillations
PIO
detector
fly‐by‐wire
url https://bjrbe.vgtu.lt/index.php/Aviation/article/view/7018
work_keys_str_mv AT pawełrzucidło thedetectionofpilotinducedoscillations
AT pawełrzucidło detectionofpilotinducedoscillations