Pitch Aircraft Control with Type-2 FLC and PD Controller

Syed Mohamad Reza Haji Mirzaie; Hodeiseh Gordan; Jalil Shirazi; Amin Nikbakht

doi:doi:10.11648/j.jeee.s.2015030201.13

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Pitch Aircraft Control with Type-2 FLC and PD Controller

Syed Mohamad Reza Haji Mirzaie, Hodeiseh Gordan, Jalil Shirazi, Amin Nikbakht

Published in Journal of Electrical and Electronic Engineering (Volume 3, Issue 2-1)

Received: 7 November 2014 Accepted: 10 November 2014 Published: 18 November 2014

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Abstract

Aircraft systems are inherently unstable systems. The equations governing the motion of an aircraft are a very complicated set of six non-linear coupled differential equations. The linearized equation around the operating point is simulated in simulink MATLAB software. Also, the linear part of the system of nonlinear equations is simulated in simulink MATLAB software. In this study, combinations of PD controllers with fuzzy controller in a unity feedback system has been employed. This paper gives a comparison between the two types of FLC type-1 and type-2 in order to show the great effect of the new type of FLCs in reducing overshoot of the step response and improving the robustness of the system.

Published in	Journal of Electrical and Electronic Engineering (Volume 3, Issue 2-1) This article belongs to the Special Issue Research and Practices in Electrical and Electronic Engineering in Developing Countries
DOI	10.11648/j.jeee.s.2015030201.13
Page(s)	12-15
Creative Commons	This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.
Copyright	Copyright © The Author(s), 2014. Published by Science Publishing Group

Keywords

PD Controller, Pitch Aircraft Angle, Type-1 Fuzzy Logic Controller, Type-2 Fuzzy Logic Controller

References

[1]	Y. John and R. Langari, Fuzzy Logic Intelligence, Control and Information. NJ: Prentice Hall, 1998.
[2]	P. King and E. Mamdani, The application of fuzzy control to industrial process, Automatica, vol. 13, pp. 235–242, 1997.
[3]	L. A. Zadeh, Outline of a new approach to analysis of complex systems and decision processes. IEEE Trans. Syst., Man, Cybern., vol. 3, no. 1, pp. 28–44, 1973.
[4]	J. M. Mendel, Rule-Based Fuzzy Logic Systems: Introduction and New Directions. NJ: Prentice-Hall, 2001.
[5]	Zadeh, L. A., The concept of a linguistic variable and its application to approximate reasoning, Part I. Information Sciences, 1975, 8(3), pp. 199–249.
[6]	Saba T. Salim, Design of Type-2 Fuzzy Logic Controller for a Simple Furnace System. Eng. & Tech. Journal, Vol.30 , No. 8, 2012
[7]	Ismail ATACAK, Design of a hybrid type-2 fuzzy logic/proportional integral controller for single-phase three-wire inverter system. Scientific Research and Essays Vol. 6(23), pp. 5049-5064, 16 October, 2011
[8]	Satish. R. Vaishnav, Zafar. J. Khan, Performance of tuned PID controller and a new hybrid fuzzy PD + I controller, World Journal of Modelling and Simulation, Vol. 6, No. 2, pp. 141-149, 2010.
[9]	M. B OZEK, Z. H. Akpolat, A Software Tool: Type-2 Fuzzy Logic Toolbox. Wiley Periodicals Inc. 2008.
[10]	A. Torabi, A. Karsaz and S. K. M. Mashhadi, “Design of Modern and Predictive Controllers for Aircraft Control System”, Latest Trends in Circuits, Systems, Signal Processing and Automatic Control, pp. 344–348, 2014.
[11]	http://ctms.engin.umich.edu/CTMS/index.php?example=AircraftPitch&section=SystemModeling

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APA Style

Syed Mohamad Reza Haji Mirzaie, Hodeiseh Gordan, Jalil Shirazi, Amin Nikbakht. (2014). Pitch Aircraft Control with Type-2 FLC and PD Controller. Journal of Electrical and Electronic Engineering, 3(2-1), 12-15. https://doi.org/10.11648/j.jeee.s.2015030201.13

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ACS Style

Syed Mohamad Reza Haji Mirzaie; Hodeiseh Gordan; Jalil Shirazi; Amin Nikbakht. Pitch Aircraft Control with Type-2 FLC and PD Controller. J. Electr. Electron. Eng. 2014, 3(2-1), 12-15. doi: 10.11648/j.jeee.s.2015030201.13

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AMA Style

Syed Mohamad Reza Haji Mirzaie, Hodeiseh Gordan, Jalil Shirazi, Amin Nikbakht. Pitch Aircraft Control with Type-2 FLC and PD Controller. J Electr Electron Eng. 2014;3(2-1):12-15. doi: 10.11648/j.jeee.s.2015030201.13

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@article{10.11648/j.jeee.s.2015030201.13,
  author = {Syed Mohamad Reza Haji Mirzaie and Hodeiseh Gordan and Jalil Shirazi and Amin Nikbakht},
  title = {Pitch Aircraft Control with Type-2 FLC and PD Controller},
  journal = {Journal of Electrical and Electronic Engineering},
  volume = {3},
  number = {2-1},
  pages = {12-15},
  doi = {10.11648/j.jeee.s.2015030201.13},
  url = {https://doi.org/10.11648/j.jeee.s.2015030201.13},
  eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.jeee.s.2015030201.13},
  abstract = {Aircraft systems are inherently unstable systems. The equations governing the motion of an aircraft are a very complicated set of six non-linear coupled differential equations. The linearized equation around the operating point is simulated in simulink MATLAB software. Also, the linear part of the system of nonlinear equations is simulated in simulink MATLAB software. In this study, combinations of PD controllers with fuzzy controller in a unity feedback system has been employed. This paper gives a comparison between the two types of FLC type-1 and type-2 in order to show the great effect of the new type of FLCs in reducing overshoot of the step response and improving the robustness of the system.},
 year = {2014}
}

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TY  - JOUR
T1  - Pitch Aircraft Control with Type-2 FLC and PD Controller
AU  - Syed Mohamad Reza Haji Mirzaie
AU  - Hodeiseh Gordan
AU  - Jalil Shirazi
AU  - Amin Nikbakht
Y1  - 2014/11/18
PY  - 2014
N1  - https://doi.org/10.11648/j.jeee.s.2015030201.13
DO  - 10.11648/j.jeee.s.2015030201.13
T2  - Journal of Electrical and Electronic Engineering
JF  - Journal of Electrical and Electronic Engineering
JO  - Journal of Electrical and Electronic Engineering
SP  - 12
EP  - 15
PB  - Science Publishing Group
SN  - 2329-1605
UR  - https://doi.org/10.11648/j.jeee.s.2015030201.13
AB  - Aircraft systems are inherently unstable systems. The equations governing the motion of an aircraft are a very complicated set of six non-linear coupled differential equations. The linearized equation around the operating point is simulated in simulink MATLAB software. Also, the linear part of the system of nonlinear equations is simulated in simulink MATLAB software. In this study, combinations of PD controllers with fuzzy controller in a unity feedback system has been employed. This paper gives a comparison between the two types of FLC type-1 and type-2 in order to show the great effect of the new type of FLCs in reducing overshoot of the step response and improving the robustness of the system.
VL  - 3
IS  - 2-1
ER  -

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Author Information

Syed Mohamad Reza Haji Mirzaie

Electrical Engineering Department, Khavaran Institute of Higher Education, Mashhad, Iran
Hodeiseh Gordan

Department of Electrical Engineering, Sobhan Institute of Higher Education, Neyshabur, Iran
Jalil Shirazi

Department of Electrical Engineering, Islamic Azad University, Gonabad Branch, Gonabad, Iran
Amin Nikbakht

Electrical Engineering Department, Khavaran Institute of Higher Education, Mashhad, Iran

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Plain Text BibTeX RIS

APA Style

Syed Mohamad Reza Haji Mirzaie, Hodeiseh Gordan, Jalil Shirazi, Amin Nikbakht. (2014). Pitch Aircraft Control with Type-2 FLC and PD Controller. Journal of Electrical and Electronic Engineering, 3(2-1), 12-15. https://doi.org/10.11648/j.jeee.s.2015030201.13

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ACS Style

Syed Mohamad Reza Haji Mirzaie; Hodeiseh Gordan; Jalil Shirazi; Amin Nikbakht. Pitch Aircraft Control with Type-2 FLC and PD Controller. J. Electr. Electron. Eng. 2014, 3(2-1), 12-15. doi: 10.11648/j.jeee.s.2015030201.13

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AMA Style

Syed Mohamad Reza Haji Mirzaie, Hodeiseh Gordan, Jalil Shirazi, Amin Nikbakht. Pitch Aircraft Control with Type-2 FLC and PD Controller. J Electr Electron Eng. 2014;3(2-1):12-15. doi: 10.11648/j.jeee.s.2015030201.13

Copy | Download

@article{10.11648/j.jeee.s.2015030201.13,
  author = {Syed Mohamad Reza Haji Mirzaie and Hodeiseh Gordan and Jalil Shirazi and Amin Nikbakht},
  title = {Pitch Aircraft Control with Type-2 FLC and PD Controller},
  journal = {Journal of Electrical and Electronic Engineering},
  volume = {3},
  number = {2-1},
  pages = {12-15},
  doi = {10.11648/j.jeee.s.2015030201.13},
  url = {https://doi.org/10.11648/j.jeee.s.2015030201.13},
  eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.jeee.s.2015030201.13},
  abstract = {Aircraft systems are inherently unstable systems. The equations governing the motion of an aircraft are a very complicated set of six non-linear coupled differential equations. The linearized equation around the operating point is simulated in simulink MATLAB software. Also, the linear part of the system of nonlinear equations is simulated in simulink MATLAB software. In this study, combinations of PD controllers with fuzzy controller in a unity feedback system has been employed. This paper gives a comparison between the two types of FLC type-1 and type-2 in order to show the great effect of the new type of FLCs in reducing overshoot of the step response and improving the robustness of the system.},
 year = {2014}
}

Copy | Download

TY  - JOUR
T1  - Pitch Aircraft Control with Type-2 FLC and PD Controller
AU  - Syed Mohamad Reza Haji Mirzaie
AU  - Hodeiseh Gordan
AU  - Jalil Shirazi
AU  - Amin Nikbakht
Y1  - 2014/11/18
PY  - 2014
N1  - https://doi.org/10.11648/j.jeee.s.2015030201.13
DO  - 10.11648/j.jeee.s.2015030201.13
T2  - Journal of Electrical and Electronic Engineering
JF  - Journal of Electrical and Electronic Engineering
JO  - Journal of Electrical and Electronic Engineering
SP  - 12
EP  - 15
PB  - Science Publishing Group
SN  - 2329-1605
UR  - https://doi.org/10.11648/j.jeee.s.2015030201.13
AB  - Aircraft systems are inherently unstable systems. The equations governing the motion of an aircraft are a very complicated set of six non-linear coupled differential equations. The linearized equation around the operating point is simulated in simulink MATLAB software. Also, the linear part of the system of nonlinear equations is simulated in simulink MATLAB software. In this study, combinations of PD controllers with fuzzy controller in a unity feedback system has been employed. This paper gives a comparison between the two types of FLC type-1 and type-2 in order to show the great effect of the new type of FLCs in reducing overshoot of the step response and improving the robustness of the system.
VL  - 3
IS  - 2-1
ER  -

Copy | Download