Detail publikace

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

KOUŘIL, M. ŠOŠOVIČKA, R. DANĚK, V. JEBÁČEK, I.

Originální název

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

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

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 aircraft 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.

Klíčová slova

aviation, aircraft, measurement

Autoři

KOUŘIL, M.; ŠOŠOVIČKA, R.; DANĚK, V.; JEBÁČEK, I.

Rok RIV

2003

Vydáno

13. 10. 2003

Nakladatel

Kaunas University of Technology

Místo

Kaunas, Litva

ISBN

9955-09-511-3

Kniha

Transport means-2003

Strany od

69

Strany do

73

Strany počet

5

BibTex

@inproceedings{BUT13306,
  author="Martin {Kouřil} and Róbert {Šošovička} and Vladimír {Daněk} and Ivo {Jebáček}",
  title="The Dynamic Measurement Unit Application for The Measurement of Light Aircraft Flight Characteristics",
  booktitle="Transport means-2003",
  year="2003",
  pages="5",
  publisher="Kaunas University of Technology",
  address="Kaunas, Litva",
  isbn="9955-09-511-3"
}