Robust level flight control design for scaled Yak-54 unmanned aerial vehicle using single sliding surface

Ussama Ali; M. Zamurad Shah; Raza Samar; Aamer Iqbal Bhatti

doi:10.1109/CCDC.2012.6244193

Robust level flight control design for scaled Yak-54 unmanned aerial vehicle using single sliding surface

Ussama Ali^*, M. Zamurad Shah, Raza Samar, Aamer Iqbal Bhatti

^*Corresponding author for this work

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

6 Scopus citations

Abstract

This paper deals with devising robust nonlinear control strategy for benchmark system of scaled Yak-54 Unmanned Aerial Vehicle. Authors considered the applications of sliding mode controllers to the longitudinal flight dynamics of the Yak-54 UAV for executing maneuvers over full flight envelope. Unlike the classical technique of the two sliding surfaces for the two loops a single surface is selected for the level flight. Control of unmanned aerial vehicle involves the problem of incomplete measurements, modeling uncertainties and external disturbances which makes flight dynamic analysis and control system design difficult. We present an innovative robust control strategy based on powerful tools provided by the theory of sliding mode control algorithms. First order sliding mode controller are designed but they provide chattering at the control input thus a non linear second order super twisting controller is used to provide chattering free control with improved robust stabilization.

Original language	English
Title of host publication	Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012
Pages	1209-1214
Number of pages	6
DOIs	https://doi.org/10.1109/CCDC.2012.6244193
State	Published - 2012
Externally published	Yes

Publication series

Name	Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012

Keywords

Higher Order Sliding Mode Control HOSM
Sliding Mode Control SMC
Strong Reachability Condition SRC

ASJC Scopus subject areas

Information Systems and Management
Control and Systems Engineering

Access to Document

10.1109/CCDC.2012.6244193

Cite this

Ali, U., Shah, M. Z., Samar, R., & Bhatti, A. I. (2012). Robust level flight control design for scaled Yak-54 unmanned aerial vehicle using single sliding surface. In Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012 (pp. 1209-1214). Article 6244193 (Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012). https://doi.org/10.1109/CCDC.2012.6244193

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title = "Robust level flight control design for scaled Yak-54 unmanned aerial vehicle using single sliding surface",

abstract = "This paper deals with devising robust nonlinear control strategy for benchmark system of scaled Yak-54 Unmanned Aerial Vehicle. Authors considered the applications of sliding mode controllers to the longitudinal flight dynamics of the Yak-54 UAV for executing maneuvers over full flight envelope. Unlike the classical technique of the two sliding surfaces for the two loops a single surface is selected for the level flight. Control of unmanned aerial vehicle involves the problem of incomplete measurements, modeling uncertainties and external disturbances which makes flight dynamic analysis and control system design difficult. We present an innovative robust control strategy based on powerful tools provided by the theory of sliding mode control algorithms. First order sliding mode controller are designed but they provide chattering at the control input thus a non linear second order super twisting controller is used to provide chattering free control with improved robust stabilization.",

keywords = "Higher Order Sliding Mode Control HOSM, Sliding Mode Control SMC, Strong Reachability Condition SRC",

author = "Ussama Ali and Shah, \{M. Zamurad\} and Raza Samar and Bhatti, \{Aamer Iqbal\}",

year = "2012",

doi = "10.1109/CCDC.2012.6244193",

language = "English",

isbn = "9781457720727",

series = "Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012",

pages = "1209--1214",

booktitle = "Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012",

}

Ali, U, Shah, MZ, Samar, R & Bhatti, AI 2012, Robust level flight control design for scaled Yak-54 unmanned aerial vehicle using single sliding surface. in Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012., 6244193, Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012, pp. 1209-1214. https://doi.org/10.1109/CCDC.2012.6244193

Robust level flight control design for scaled Yak-54 unmanned aerial vehicle using single sliding surface. / Ali, Ussama; Shah, M. Zamurad; Samar, Raza et al.
Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012. 2012. p. 1209-1214 6244193 (Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012).

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

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T1 - Robust level flight control design for scaled Yak-54 unmanned aerial vehicle using single sliding surface

AU - Ali, Ussama

AU - Shah, M. Zamurad

AU - Samar, Raza

AU - Bhatti, Aamer Iqbal

PY - 2012

Y1 - 2012

N2 - This paper deals with devising robust nonlinear control strategy for benchmark system of scaled Yak-54 Unmanned Aerial Vehicle. Authors considered the applications of sliding mode controllers to the longitudinal flight dynamics of the Yak-54 UAV for executing maneuvers over full flight envelope. Unlike the classical technique of the two sliding surfaces for the two loops a single surface is selected for the level flight. Control of unmanned aerial vehicle involves the problem of incomplete measurements, modeling uncertainties and external disturbances which makes flight dynamic analysis and control system design difficult. We present an innovative robust control strategy based on powerful tools provided by the theory of sliding mode control algorithms. First order sliding mode controller are designed but they provide chattering at the control input thus a non linear second order super twisting controller is used to provide chattering free control with improved robust stabilization.

AB - This paper deals with devising robust nonlinear control strategy for benchmark system of scaled Yak-54 Unmanned Aerial Vehicle. Authors considered the applications of sliding mode controllers to the longitudinal flight dynamics of the Yak-54 UAV for executing maneuvers over full flight envelope. Unlike the classical technique of the two sliding surfaces for the two loops a single surface is selected for the level flight. Control of unmanned aerial vehicle involves the problem of incomplete measurements, modeling uncertainties and external disturbances which makes flight dynamic analysis and control system design difficult. We present an innovative robust control strategy based on powerful tools provided by the theory of sliding mode control algorithms. First order sliding mode controller are designed but they provide chattering at the control input thus a non linear second order super twisting controller is used to provide chattering free control with improved robust stabilization.

KW - Higher Order Sliding Mode Control HOSM

KW - Sliding Mode Control SMC

KW - Strong Reachability Condition SRC

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T3 - Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012

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BT - Proceedings of the 2012 24th Chinese Control and Decision Conference, CCDC 2012

ER -

Robust level flight control design for scaled Yak-54 unmanned aerial vehicle using single sliding surface

Abstract

Publication series

Keywords

ASJC Scopus subject areas

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