Detail publikace

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

KOUŘIL, M.

Originální název

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

Typ

článek v časopise - ostatní, Jost

Jazyk

angličtina

Originální abstrakt

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-directional 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.

Klíčová slova

flight characteristics, aerodynamics

Autoři

KOUŘIL, M.

Rok RIV

2004

Vydáno

18. 12. 2003

ISSN

1648-7788

Periodikum

AVIATION

Ročník

2003

Číslo

3

Stát

Litevská republika

Strany od

37

Strany do

44

Strany počet

8

BibTex

@article{BUT41952,
  author="Martin {Kouřil}",
  title="The Dynamic Stability Analysis of the Next Generation Airplane for Pilot Training",
  journal="AVIATION",
  year="2003",
  volume="2003",
  number="3",
  pages="8",
  issn="1648-7788"
}