Publication detail

Analysis of the Dynamic Properties of Longitudinal Flight Based on the Measurement on the Flight Simulator

JIRGL, M. JALOVECKÝ, R.

Original Title

Analysis of the Dynamic Properties of Longitudinal Flight Based on the Measurement on the Flight Simulator

English Title

Analysis of the Dynamic Properties of Longitudinal Flight Based on the Measurement on the Flight Simulator

Type

journal article

Language

en

Original Abstract

This paper deals with an analysis of dynamic properties of aircraft longitudinal flight. This analysis is based on the measurement of the longitudinal flight model parameters using flight simulator. There are measured responses of aircraft on change of the input signal. Identification of longitudinal flight model parameters follows after these measurements. The identified models are used for analysis of dynamic properties of longitudinal flight.

English abstract

This paper deals with an analysis of dynamic properties of aircraft longitudinal flight. This analysis is based on the measurement of the longitudinal flight model parameters using flight simulator. There are measured responses of aircraft on change of the input signal. Identification of longitudinal flight model parameters follows after these measurements. The identified models are used for analysis of dynamic properties of longitudinal flight.

Keywords

longitudinal flight, flight simulator, XPLANE-10, MATLAB, dynamic properties of longitudinal flight

RIV year

2015

Released

22.10.2015

Location

Lithuania

Pages from

290

Pages to

293

Pages count

4

BibTex


@article{BUT117975,
  author="Miroslav {Jirgl} and Rudolf {Jalovecký}",
  title="Analysis of the Dynamic Properties of Longitudinal Flight Based on the Measurement on the Flight Simulator",
  annote="This paper deals with an analysis of dynamic properties of aircraft longitudinal flight. This analysis is based on the measurement of the longitudinal flight model parameters using flight simulator. There are measured responses of aircraft on change of the input signal. Identification of longitudinal flight model parameters follows after these measurements. The identified models are used for analysis of dynamic properties of longitudinal flight.",
  chapter="117975",
  howpublished="electronic, physical medium",
  number="1",
  year="2015",
  month="october",
  pages="290--293",
  type="journal article"
}