Analýza dynamické stability lehkého letounu nové generace

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F03%3APU41994" target="_blank" >RIV/00216305:26210/03:PU41994 - isvavai.cz</a>

Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

The Dynamic Stability Analysis of the Next Generation Airplane for Pilot Training

Popis výsledku v původním jazyce

The stability and controllability of an airplane are essential parts of the evaluation of the airplane complex flight characteristics. Therefore, more and more demands during airplane development are put on its stability computation from its early design. The stability and controllability is influencing not only the airplane total layout but, nowadays, also safety of flight operation and passenger comfort in airliner. The inference non-dimensional linearized equations for longitudinal and lateral-directtional motion of airplane are modelled in the computation and program system Matlab and modelling, simulating system Simulink. The created computer program is determined for the calculation the dynamic stability light airplane with free-control or fix-control. The calculation is applied for light airplane of new generation VUT 100.

Název v anglickém jazyce

The Dynamic Stability Analysis of the Next Generation Airplane for Pilot Training

Popis výsledku anglicky

The stability and controllability of an airplane are essential parts of the evaluation of the airplane complex flight characteristics. Therefore, more and more demands during airplane development are put on its stability computation from its early design. The stability and controllability is influencing not only the airplane total layout but, nowadays, also safety of flight operation and passenger comfort in airliner. The inference non-dimensional linearized equations for longitudinal and lateral-directtional motion of airplane are modelled in the computation and program system Matlab and modelling, simulating system Simulink. The created computer program is determined for the calculation the dynamic stability light airplane with free-control or fix-control. The calculation is applied for light airplane of new generation VUT 100.

Druh

J_x - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

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Návaznosti

Z - Vyzkumny zamer (s odkazem do CEZ)

Rok uplatnění

2003

Kód důvěrnosti údajů

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

Název periodika

AVIATION

ISSN

1648-7788

e-ISSN

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Svazek periodika

2003

Číslo periodika v rámci svazku

3

Stát vydavatele periodika

LT - Litevská republika

Počet stran výsledku

8

Strana od-do

37-44

Kód UT WoS článku

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EID výsledku v databázi Scopus

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