Publication detail

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

KOUŘIL, M.

Czech title

Analýza dynamické stability lehkého letounu nové generace

English title

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

Type

journal article - other

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.

Czech abstract

Stabilita a řiditelnost letounu jsou neodmyslitelnou součástí hodnocení komplexních letových vlastností letounu. Proto se na výpočet stability letounu klade stále více nároků při vývoji letounu. Stabilita a řiditelnost ovlivňuje nejen celkovou koncepci navrhovaného letounu, ale v dnešní době i bezpečnost letového provozu a hlavně u dopravních letounů komfort cestujících. Odvozené bezrozměrové linearizované rovnice podélného a stranového pohybu letounu jsou namodelovány ve výpočtovém a programovém systému Matlab a simulačním systému Simulink. Vytvořený program je určen pro výpočet dynamické stability lehkého letounu s volným a pevným řízením. Výpočet je aplikován na lehký letoun nové generace VUT 100.

English 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 Czech

letové vlastnosti, aerodynamika

Keywords in English

flight characteristics, aerodynamics

RIV year

2004

Released

18.12.2003

ISSN

1648-7788

Journal

AVIATION

Volume

2003

Number

3

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",
  month="December",
  issn="1648-7788"
}