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Reducing the Effect of the Atmospheric Disturbance on Longitudinal Fight Control System Usage PID Controller

by Muna Hadi Saleh, Noor Abdul Razzaq Raheem
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International Journal of Computer Applications
Foundation of Computer Science (FCS), NY, USA
Volume 127 - Number 13
Year of Publication: 2015
Authors: Muna Hadi Saleh, Noor Abdul Razzaq Raheem
10.5120/ijca2015906586

Muna Hadi Saleh, Noor Abdul Razzaq Raheem . Reducing the Effect of the Atmospheric Disturbance on Longitudinal Fight Control System Usage PID Controller. International Journal of Computer Applications. 127, 13 ( October 2015), 27-31. DOI=10.5120/ijca2015906586

@article{ 10.5120/ijca2015906586,
author = { Muna Hadi Saleh, Noor Abdul Razzaq Raheem },
title = { Reducing the Effect of the Atmospheric Disturbance on Longitudinal Fight Control System Usage PID Controller },
journal = { International Journal of Computer Applications },
issue_date = { October 2015 },
volume = { 127 },
number = { 13 },
month = { October },
year = { 2015 },
issn = { 0975-8887 },
pages = { 27-31 },
numpages = {9},
url = { https://ijcaonline.org/archives/volume127/number13/22791-2015906586/ },
doi = { 10.5120/ijca2015906586 },
publisher = {Foundation of Computer Science (FCS), NY, USA},
address = {New York, USA}
}
%0 Journal Article
%1 2024-02-06T23:19:50.056489+05:30
%A Muna Hadi Saleh
%A Noor Abdul Razzaq Raheem
%T Reducing the Effect of the Atmospheric Disturbance on Longitudinal Fight Control System Usage PID Controller
%J International Journal of Computer Applications
%@ 0975-8887
%V 127
%N 13
%P 27-31
%D 2015
%I Foundation of Computer Science (FCS), NY, USA
Abstract

Autopilot systems have been vital to flight control for several years and have been making flight easier and more effective. Nevertheless, these autopilot systems are complex devices that demand exact control and stability. In this paper, design PID controller to control pitch angle in longitudinal dynamic of the autopilot system for jet transport using MATLAB/SIMULINK. In this paper designed on automatic pilot with Multi Input Multi Output (MIMO) system. Also, we studied the effect of atmospheric disturbances when a PID controller has been applied the results shown how this controller with good tuning reducing the effect of atmospheric disturbance on the consistency of the autopilot.

References
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  2. K. Turkoglu, U. Ozdemir, M. Nikbay, E. Jafarov. 2008. PID parameter optimization of a UAV longitudinal Flight Control system. World Academy of Science, Engineering and Technology.
  3. Rauw, Marc. 2001. A Simulink Toolbox for Flight Dynamics and Control Analysis. Marc Rauw.
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  7. Uma in Ahsun. 1996. Dynamic characterization and Active Control of Unstarts in a Near-Isentropic Supersonic Intet. Lahore Pakistan.
  8. B. Kada, Y. Ghazzawi.2011. Robust PID Controller Design for an UAV Flight Control System. San Francisco, USA.
  9. Ashish Tewari. 2007. Atmospheric and Space Flight Dynamics Modeling and Simulation with meth lab and Simulink. Birkhauser Boston.
Index Terms

Computer Science
Information Sciences

Keywords

Longitudinal Autopilot Pitch angle Atmospheric Disturbance Flight Control PID

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