Effect of the Pilot Behavior Model on the Helicopter Stability in the Auto-Stabilization System Failure

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F12%3A00477213" target="_blank" >RIV/60162694:G43__/12:00477213 - isvavai.cz</a>

Result on the web

<a href="http://vavtest.unob.cz/registr" target="_blank" >http://vavtest.unob.cz/registr</a>

DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Effect of the Pilot Behavior Model on the Helicopter Stability in the Auto-Stabilization System Failure

Original language description

This paper describes a mathematical identification of time constants for pilot behavior during a helicopter control process. Based on this mathematical identification and a mathematical description of helicopter dynamics, a simulation scheme was built inthe Simulink? environment. Subsequently, the analysis of time constant changes in a pilot behavior model during helicopter longitudinal motion was done, including changes in transfer delay as well as in pilot?s gain. The obtained results are presented in the selected examples in the form of 3D graphs, all created in MATLAB?.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

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Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2012

Confidentiality

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

Article name in the collection

ESTEL 2012 Proceedings

ISBN

978-1-4673-4688-7

ISSN

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e-ISSN

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Number of pages

4

Pages from-to

1-4

Publisher name

Neuveden

Place of publication

Italy

Event location

Rome-Italy

Event date

Jan 1, 2012

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

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