Detail publikace

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

KOUŘIL, M.

Anglický název

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

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

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 anglicky

flight characteristics, aerodynamics

Vydáno

2003-12-18

ISSN

1648-7788

Časopis

Aviation

Ročník

2003

Číslo

3

Strany od–do

37–

Počet stran

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"
}