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Development of a Longitudinal Control Model of an Aircraft with Gusty Environment

by Noor Thamer Almalah, Huda Aqeel Al-Tayyar
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International Journal of Computer Applications
Foundation of Computer Science (FCS), NY, USA
Volume 176 - Number 38
Year of Publication: 2020
Authors: Noor Thamer Almalah, Huda Aqeel Al-Tayyar
10.5120/ijca2020920464

Noor Thamer Almalah, Huda Aqeel Al-Tayyar . Development of a Longitudinal Control Model of an Aircraft with Gusty Environment. International Journal of Computer Applications. 176, 38 ( Jul 2020), 29-33. DOI=10.5120/ijca2020920464

@article{ 10.5120/ijca2020920464,
author = { Noor Thamer Almalah, Huda Aqeel Al-Tayyar },
title = { Development of a Longitudinal Control Model of an Aircraft with Gusty Environment },
journal = { International Journal of Computer Applications },
issue_date = { Jul 2020 },
volume = { 176 },
number = { 38 },
month = { Jul },
year = { 2020 },
issn = { 0975-8887 },
pages = { 29-33 },
numpages = {9},
url = { https://ijcaonline.org/archives/volume176/number38/31452-2020920464/ },
doi = { 10.5120/ijca2020920464 },
publisher = {Foundation of Computer Science (FCS), NY, USA},
address = {New York, USA}
}
%0 Journal Article
%1 2024-02-07T00:44:32.269913+05:30
%A Noor Thamer Almalah
%A Huda Aqeel Al-Tayyar
%T Development of a Longitudinal Control Model of an Aircraft with Gusty Environment
%J International Journal of Computer Applications
%@ 0975-8887
%V 176
%N 38
%P 29-33
%D 2020
%I Foundation of Computer Science (FCS), NY, USA
Abstract

The humanity fascination about aerodynamic flight system and the fantasy of air flying have induced the hesitating understanding of elementary aerodynamic phenomena. The controller system considered the heart of aerodynamic motion since taking off till landing. The obvious compatibility between the output and the input is the aim of this study. This paper has contributed toward the development of a control system in aircrafts and has indicated especially how to design a longitudinal flight control for aircrafts. The stick commands of a pilot can be applied as the set level for the aircraft situation , angle of direction, and pitch rate to determine commands. The results displayed a good output corresponding to input (stick command) after a significant changes in model transfer functions. This mean it has been reached to design a controller model with an impact filters to get a best response of the aircraft motion depending on what a pilot commands. Finally, a modified Dryden wind gust structure has merged to destabilize the system and bring closer approach into a real environment.

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Index Terms

Computer Science
Information Sciences

Keywords

Flight control Longitudinal Aerodynamic Dryden wind gust Pilot stick

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