Publication detail

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

KOUŘIL, M.

English title

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

Type

Peer-reviewed article not indexed in WoS or Scopus

Language

en

Original abstract

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.

Keywords in English

flight characteristics, aerodynamics

Released

2003-12-18

ISSN

1648-7788

Journal

Aviation

Volume

2003

Number

3

Pages from–to

37–

Pages count

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"
}