Conventional PID, adaptive PID, and sliding mode controllers design for aircraft pitch control

Adnan Khalid; Kamran Zeb; Aun Haider

doi:10.1109/CEET1.2019.8711871

Conventional PID, adaptive PID, and sliding mode controllers design for aircraft pitch control

Adnan Khalid, Kamran Zeb, Aun Haider

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

24 Scopus citations

Abstract

In this paper conventional PID, Fuzzy PID and Sliding Mode (SM) controllers have been designed and analyzed for the pitch control of an aircraft. The main purpose is to stabilize the aircraft in case of any external disturbance. An appropriate mathematical model for the longitudinal motion of aircraft is considered. Simulations are performed in MATLAB Simulink for the proposed controllers and results are critically and analytically discussed. Furthermore, analysis based on different performance measures i.e. Integral Squared Error (ISE), Integral Absolute Error (IAE), rise time, settling time, and under shoot are performed to compare the response of the controllers. Besides in comparison, the simulation results validate the robustness and better performance of SMC and Fuzzy PID for pitch control of an aircraft.

Original language	English
Title of host publication	2019 International Conference on Engineering and Emerging Technologies, ICEET 2019
Publisher	Institute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)	9781538621707
DOIs	https://doi.org/10.1109/CEET1.2019.8711871
State	Published - 9 May 2019
Externally published	Yes
Event	2019 International Conference on Engineering and Emerging Technologies, ICEET 2019 - Lahore, Pakistan Duration: 21 Feb 2019 → 22 Feb 2019

Publication series

Name	2019 International Conference on Engineering and Emerging Technologies, ICEET 2019

Conference

Conference	2019 International Conference on Engineering and Emerging Technologies, ICEET 2019
Country/Territory	Pakistan
City	Lahore
Period	21/02/19 → 22/02/19

Bibliographical note

Publisher Copyright:
© 2019 IEEE.

Keywords

Aircraft pitch control
Fuzzy PID
Integral Squared Error and Integral Absolute Error
PID
Sliding Mode Control

ASJC Scopus subject areas

Signal Processing
Computer Networks and Communications
Hardware and Architecture
Energy Engineering and Power Technology
Control and Systems Engineering
Electrical and Electronic Engineering

Access to Document

10.1109/CEET1.2019.8711871

Cite this

Khalid, A., Zeb, K., & Haider, A. (2019). Conventional PID, adaptive PID, and sliding mode controllers design for aircraft pitch control. In 2019 International Conference on Engineering and Emerging Technologies, ICEET 2019 Article 8711871 (2019 International Conference on Engineering and Emerging Technologies, ICEET 2019). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CEET1.2019.8711871

Khalid, Adnan ; Zeb, Kamran ; Haider, Aun. / Conventional PID, adaptive PID, and sliding mode controllers design for aircraft pitch control. 2019 International Conference on Engineering and Emerging Technologies, ICEET 2019. Institute of Electrical and Electronics Engineers Inc., 2019. (2019 International Conference on Engineering and Emerging Technologies, ICEET 2019).

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title = "Conventional PID, adaptive PID, and sliding mode controllers design for aircraft pitch control",

abstract = "In this paper conventional PID, Fuzzy PID and Sliding Mode (SM) controllers have been designed and analyzed for the pitch control of an aircraft. The main purpose is to stabilize the aircraft in case of any external disturbance. An appropriate mathematical model for the longitudinal motion of aircraft is considered. Simulations are performed in MATLAB Simulink for the proposed controllers and results are critically and analytically discussed. Furthermore, analysis based on different performance measures i.e. Integral Squared Error (ISE), Integral Absolute Error (IAE), rise time, settling time, and under shoot are performed to compare the response of the controllers. Besides in comparison, the simulation results validate the robustness and better performance of SMC and Fuzzy PID for pitch control of an aircraft.",

keywords = "Aircraft pitch control, Fuzzy PID, Integral Squared Error and Integral Absolute Error, PID, Sliding Mode Control",

author = "Adnan Khalid and Kamran Zeb and Aun Haider",

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year = "2019",

month = may,

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doi = "10.1109/CEET1.2019.8711871",

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Khalid, A, Zeb, K & Haider, A 2019, Conventional PID, adaptive PID, and sliding mode controllers design for aircraft pitch control. in 2019 International Conference on Engineering and Emerging Technologies, ICEET 2019., 8711871, 2019 International Conference on Engineering and Emerging Technologies, ICEET 2019, Institute of Electrical and Electronics Engineers Inc., 2019 International Conference on Engineering and Emerging Technologies, ICEET 2019, Lahore, Pakistan, 21/02/19. https://doi.org/10.1109/CEET1.2019.8711871

Conventional PID, adaptive PID, and sliding mode controllers design for aircraft pitch control. / Khalid, Adnan; Zeb, Kamran; Haider, Aun.
2019 International Conference on Engineering and Emerging Technologies, ICEET 2019. Institute of Electrical and Electronics Engineers Inc., 2019. 8711871 (2019 International Conference on Engineering and Emerging Technologies, ICEET 2019).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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N2 - In this paper conventional PID, Fuzzy PID and Sliding Mode (SM) controllers have been designed and analyzed for the pitch control of an aircraft. The main purpose is to stabilize the aircraft in case of any external disturbance. An appropriate mathematical model for the longitudinal motion of aircraft is considered. Simulations are performed in MATLAB Simulink for the proposed controllers and results are critically and analytically discussed. Furthermore, analysis based on different performance measures i.e. Integral Squared Error (ISE), Integral Absolute Error (IAE), rise time, settling time, and under shoot are performed to compare the response of the controllers. Besides in comparison, the simulation results validate the robustness and better performance of SMC and Fuzzy PID for pitch control of an aircraft.

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Khalid A, Zeb K, Haider A. Conventional PID, adaptive PID, and sliding mode controllers design for aircraft pitch control. In 2019 International Conference on Engineering and Emerging Technologies, ICEET 2019. Institute of Electrical and Electronics Engineers Inc. 2019. 8711871. (2019 International Conference on Engineering and Emerging Technologies, ICEET 2019). doi: 10.1109/CEET1.2019.8711871

Conventional PID, adaptive PID, and sliding mode controllers design for aircraft pitch control

Abstract

Publication series

Conference

Bibliographical note

Keywords

ASJC Scopus subject areas

Access to Document

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Cite this