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

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F03%3APU42020" target="_blank" >RIV/00216305:26210/03:PU42020 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

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

Original language description

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.

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

Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year

2003

Confidentiality

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

Article name in the collection

Transport means-2003

ISBN

9955-09-511-3

ISSN

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e-ISSN

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Number of pages

5

Pages from-to

69-73

Publisher name

Kaunas University of Technology

Place of publication

Kaunas, Litva

Event location

Litva

Event date

Jan 1, 2001

Type of event by nationality

EUR - Evropská akce

UT code for WoS article

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