Landing of Aircraft Using Integral State Feedback Sliding Mode Control

Ahmad Mahmood; Aamer Iqbal Bhatti; Bilal A. Siddique

doi:10.1109/ICECCE47252.2019.8940802

Landing of Aircraft Using Integral State Feedback Sliding Mode Control

Ahmad Mahmood
, Aamer Iqbal Bhatti
, Bilal A. Siddique

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

7 Scopus citations

Abstract

Landing is daunting control design problem because it demands high accuracy and precision by pilot. Among the various states to control for stability and landing in an Aircraft, one is its altitude to handle during landing. Since the linearized model of aircraft is considered and is used for altitude control design. For best tracking performance during glide and flare phase, Integral State feedback Sliding Mode Control (ISSMC) is applied, which is based on unit vector approach. To eliminate error between responded altitude and referenced altitude, a dynamic demand first order filter is used. There has been noted a significant improvement in performance as compared with PID control. When comparing the Integral State feedback Sliding Mode Control with PID during landing phase, the ISSMC yields the best response of glide and flare maneuverability for smooth touch down during landing on runway.

Original language	English
Title of host publication	1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019
Publisher	Institute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)	9781728138251
DOIs	https://doi.org/10.1109/ICECCE47252.2019.8940802
State	Published - Jul 2019
Externally published	Yes
Event	1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019 - Swat, Pakistan Duration: 24 Jul 2019 → 25 Jul 2019

Publication series

Name	1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019

Conference

Conference	1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019
Country/Territory	Pakistan
City	Swat
Period	24/07/19 → 25/07/19

Bibliographical note

Publisher Copyright:
© 2019 IEEE.

Keywords

ISSMC
PID
flare path
glide path
landing

ASJC Scopus subject areas

Artificial Intelligence
Computer Networks and Communications
Computer Vision and Pattern Recognition
Hardware and Architecture
Electrical and Electronic Engineering
Energy Engineering and Power Technology
Renewable Energy, Sustainability and the Environment
Control and Optimization

Access to Document

10.1109/ICECCE47252.2019.8940802

Cite this

Mahmood, A., Bhatti, A. I., & Siddique, B. A. (2019). Landing of Aircraft Using Integral State Feedback Sliding Mode Control. In 1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019 Article 8940802 (1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICECCE47252.2019.8940802

Mahmood, Ahmad ; Bhatti, Aamer Iqbal ; Siddique, Bilal A. / Landing of Aircraft Using Integral State Feedback Sliding Mode Control. 1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019. Institute of Electrical and Electronics Engineers Inc., 2019. (1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019).

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title = "Landing of Aircraft Using Integral State Feedback Sliding Mode Control",

abstract = "Landing is daunting control design problem because it demands high accuracy and precision by pilot. Among the various states to control for stability and landing in an Aircraft, one is its altitude to handle during landing. Since the linearized model of aircraft is considered and is used for altitude control design. For best tracking performance during glide and flare phase, Integral State feedback Sliding Mode Control (ISSMC) is applied, which is based on unit vector approach. To eliminate error between responded altitude and referenced altitude, a dynamic demand first order filter is used. There has been noted a significant improvement in performance as compared with PID control. When comparing the Integral State feedback Sliding Mode Control with PID during landing phase, the ISSMC yields the best response of glide and flare maneuverability for smooth touch down during landing on runway.",

keywords = "ISSMC, PID, flare path, glide path, landing",

author = "Ahmad Mahmood and Bhatti, \{Aamer Iqbal\} and Siddique, \{Bilal A.\}",

note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019 ; Conference date: 24-07-2019 Through 25-07-2019",

year = "2019",

month = jul,

doi = "10.1109/ICECCE47252.2019.8940802",

language = "English",

series = "1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

booktitle = "1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019",

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Mahmood, A, Bhatti, AI & Siddique, BA 2019, Landing of Aircraft Using Integral State Feedback Sliding Mode Control. in 1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019., 8940802, 1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019, Institute of Electrical and Electronics Engineers Inc., 1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019, Swat, Pakistan, 24/07/19. https://doi.org/10.1109/ICECCE47252.2019.8940802

Landing of Aircraft Using Integral State Feedback Sliding Mode Control. / Mahmood, Ahmad; Bhatti, Aamer Iqbal; Siddique, Bilal A.
1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019. Institute of Electrical and Electronics Engineers Inc., 2019. 8940802 (1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019).

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

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AU - Bhatti, Aamer Iqbal

AU - Siddique, Bilal A.

PY - 2019/7

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N2 - Landing is daunting control design problem because it demands high accuracy and precision by pilot. Among the various states to control for stability and landing in an Aircraft, one is its altitude to handle during landing. Since the linearized model of aircraft is considered and is used for altitude control design. For best tracking performance during glide and flare phase, Integral State feedback Sliding Mode Control (ISSMC) is applied, which is based on unit vector approach. To eliminate error between responded altitude and referenced altitude, a dynamic demand first order filter is used. There has been noted a significant improvement in performance as compared with PID control. When comparing the Integral State feedback Sliding Mode Control with PID during landing phase, the ISSMC yields the best response of glide and flare maneuverability for smooth touch down during landing on runway.

AB - Landing is daunting control design problem because it demands high accuracy and precision by pilot. Among the various states to control for stability and landing in an Aircraft, one is its altitude to handle during landing. Since the linearized model of aircraft is considered and is used for altitude control design. For best tracking performance during glide and flare phase, Integral State feedback Sliding Mode Control (ISSMC) is applied, which is based on unit vector approach. To eliminate error between responded altitude and referenced altitude, a dynamic demand first order filter is used. There has been noted a significant improvement in performance as compared with PID control. When comparing the Integral State feedback Sliding Mode Control with PID during landing phase, the ISSMC yields the best response of glide and flare maneuverability for smooth touch down during landing on runway.

KW - ISSMC

KW - PID

KW - flare path

KW - glide path

KW - landing

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M3 - Conference contribution

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T3 - 1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019

BT - 1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019

PB - Institute of Electrical and Electronics Engineers Inc.

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Mahmood A, Bhatti AI, Siddique BA. Landing of Aircraft Using Integral State Feedback Sliding Mode Control. In 1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019. Institute of Electrical and Electronics Engineers Inc. 2019. 8940802. (1st International Conference on Electrical, Communication and Computer Engineering, ICECCE 2019). doi: 10.1109/ICECCE47252.2019.8940802

Landing of Aircraft Using Integral State Feedback Sliding Mode Control

Abstract

Publication series

Conference

Bibliographical note

Keywords

ASJC Scopus subject areas

Access to Document

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Cite this