Finite-time path following control for a stratospheric airship with input saturation and error constraint

This paper addresses the finite-time path following control problem for an under-actuated stratospheric airship with input saturation, error constraint, and external disturbances. To handle the adverse effect of input saturation, anti-windup compensators are employed and finite-time convergence of t...

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Main Authors: Zheng, Zewei, Xie, Lihua
Other Authors: School of Electrical and Electronic Engineering
Format: Article
Language:English
Published: 2021
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Online Access:https://hdl.handle.net/10356/151371
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1513712021-06-15T03:23:18Z Finite-time path following control for a stratospheric airship with input saturation and error constraint Zheng, Zewei Xie, Lihua School of Electrical and Electronic Engineering Engineering::Electrical and electronic engineering Stratospheric Airship Finite-time Control This paper addresses the finite-time path following control problem for an under-actuated stratospheric airship with input saturation, error constraint, and external disturbances. To handle the adverse effect of input saturation, anti-windup compensators are employed and finite-time convergence of the saturated control solution is established. Error constraints of airship position and attitude are handled by incorporating a tan-type barrier Lyapunov function (TBLF) in guidance and attitude control schemes. Backstepping design is presented with the anti-windup compensators, the TBLF, and nonlinear disturbance observers which estimate the external disturbances. Stability analysis shows that the tracking errors of the airship position converge into a small set around zero within finite-time, the constrained requirements on the airship position and attitude are not violated during operation, and all closed-loop signals are guaranteed to be uniformly ultimately bounded. Compared with the conventional control scheme, simulation results illustrate that the proposed finite-time controller offers a faster convergence rate and a higher path following accuracy for the stratospheric airship. This work was supported in part by the National Natural Science Foundation of China [grant number 61503010], [grant number 61673034]; Aeronautical Science Foundation of China [grant number 2016ZA51001]; National Key R&D Program of China [grant number 2016YFB1200100]; Fundamental Research Funds for the Central Universities [grant number YWF-16-GJSYS-02]. The work of Zewei Zheng was supported by the China Scholarship Council [grant number 201606025076]. 2021-06-15T03:23:18Z 2021-06-15T03:23:18Z 2019 Journal Article Zheng, Z. & Xie, L. (2019). Finite-time path following control for a stratospheric airship with input saturation and error constraint. International Journal of Control, 92(2), 368-393. https://dx.doi.org/10.1080/00207179.2017.1357839 0020-7179 0000-0001-9412-4271 https://hdl.handle.net/10356/151371 10.1080/00207179.2017.1357839 2-s2.0-85027007926 2 92 368 393 en International Journal of Control © 2017 Informa UK Limited, trading as Taylor & Francis Group. All rights reserved.
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Electrical and electronic engineering
Stratospheric Airship
Finite-time Control
spellingShingle Engineering::Electrical and electronic engineering
Stratospheric Airship
Finite-time Control
Zheng, Zewei
Xie, Lihua
Finite-time path following control for a stratospheric airship with input saturation and error constraint
description This paper addresses the finite-time path following control problem for an under-actuated stratospheric airship with input saturation, error constraint, and external disturbances. To handle the adverse effect of input saturation, anti-windup compensators are employed and finite-time convergence of the saturated control solution is established. Error constraints of airship position and attitude are handled by incorporating a tan-type barrier Lyapunov function (TBLF) in guidance and attitude control schemes. Backstepping design is presented with the anti-windup compensators, the TBLF, and nonlinear disturbance observers which estimate the external disturbances. Stability analysis shows that the tracking errors of the airship position converge into a small set around zero within finite-time, the constrained requirements on the airship position and attitude are not violated during operation, and all closed-loop signals are guaranteed to be uniformly ultimately bounded. Compared with the conventional control scheme, simulation results illustrate that the proposed finite-time controller offers a faster convergence rate and a higher path following accuracy for the stratospheric airship.
author2 School of Electrical and Electronic Engineering
author_facet School of Electrical and Electronic Engineering
Zheng, Zewei
Xie, Lihua
format Article
author Zheng, Zewei
Xie, Lihua
author_sort Zheng, Zewei
title Finite-time path following control for a stratospheric airship with input saturation and error constraint
title_short Finite-time path following control for a stratospheric airship with input saturation and error constraint
title_full Finite-time path following control for a stratospheric airship with input saturation and error constraint
title_fullStr Finite-time path following control for a stratospheric airship with input saturation and error constraint
title_full_unstemmed Finite-time path following control for a stratospheric airship with input saturation and error constraint
title_sort finite-time path following control for a stratospheric airship with input saturation and error constraint
publishDate 2021
url https://hdl.handle.net/10356/151371
_version_ 1703971191746723840