The Dynamic Measurement Unit Application for The Measurement of Light Aircraft Flight Characteristics

Kód výsledku v IS VaVaI

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Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

The Dynamic Measurement Unit Application for The Measurement of Light Aircraft Flight Characteristics

Popis výsledku v původním jazyce

This paper presents the application of modern equipment (optical gyro) at flight measurement of light aircraft. The paper is dealing in detail with performed measurements of longitudinal dynamic stability of aircraft. Dynamic stability control presents one of the important parts of flight characteristics analysis of atmospheric aircraft. The dynamic stability calculations, following aircraft from its primary design, have great influence on the final aircraft appearance. The suitability of proposed aircrraft design, and possible modifications, will appear just during the flight tests. The results of tests are used for the verification of designed aircraft stability and control and for the verification of applied theory as well.

Název v anglickém jazyce

The Dynamic Measurement Unit Application for The Measurement of Light Aircraft Flight Characteristics

Popis výsledku anglicky

This paper presents the application of modern equipment (optical gyro) at flight measurement of light aircraft. The paper is dealing in detail with performed measurements of longitudinal dynamic stability of aircraft. Dynamic stability control presents one of the important parts of flight characteristics analysis of atmospheric aircraft. The dynamic stability calculations, following aircraft from its primary design, have great influence on the final aircraft appearance. The suitability of proposed aircrraft design, and possible modifications, will appear just during the flight tests. The results of tests are used for the verification of designed aircraft stability and control and for the verification of applied theory as well.

Druh

D - Stať ve sborníku

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 statě ve sborníku

Transport means-2003

ISBN

9955-09-511-3

ISSN

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e-ISSN

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Počet stran výsledku

5

Strana od-do

69-73

Název nakladatele

Kaunas University of Technology

Místo vydání

Kaunas, Litva

Místo konání akce

Litva

Datum konání akce

1. 1. 2001

Typ akce podle státní příslušnosti

EUR - Evropská akce

Kód UT WoS článku

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