Nonsingular Fast Terminal Adaptive Neuro-sliding Mode Control for Spacecraft Formation Flying Systems

In this paper, a nonsingular fast terminal adaptive neurosliding mode control for spacecraft formation flying systems is investigated. First, a supertwisting disturbance observer is employed to estimate external disturbances in the system. Second, a fast nonsingular terminal sliding mode control law...

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Main Authors: Xiaohan Lin, Xiaoping Shi, Shilun Li, Sing Kiong Nguang, Liruo Zhang
Format: Article
Language:English
Published: Wiley 2020-01-01
Series:Complexity
Online Access:http://dx.doi.org/10.1155/2020/5875191
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author Xiaohan Lin
Xiaoping Shi
Shilun Li
Sing Kiong Nguang
Liruo Zhang
author_facet Xiaohan Lin
Xiaoping Shi
Shilun Li
Sing Kiong Nguang
Liruo Zhang
author_sort Xiaohan Lin
collection DOAJ
description In this paper, a nonsingular fast terminal adaptive neurosliding mode control for spacecraft formation flying systems is investigated. First, a supertwisting disturbance observer is employed to estimate external disturbances in the system. Second, a fast nonsingular terminal sliding mode control law is proposed to guarantee the tracking errors of the spacecraft formation converge to zero in finite time. Third, for the unknown parts in the spacecraft formation flying dynamics, we proposed an adaptive neurosliding mode control law to compensate them. The proposed sliding mode control laws not only achieve the formation but also alleviate the effect of the chattering. Finally, simulations are used to demonstrate the effectiveness of the proposed control laws.
format Article
id doaj-art-01641bd23d2a42efaaeee4987c7cccb1
institution Kabale University
issn 1076-2787
1099-0526
language English
publishDate 2020-01-01
publisher Wiley
record_format Article
series Complexity
spelling doaj-art-01641bd23d2a42efaaeee4987c7cccb12025-08-20T03:55:24ZengWileyComplexity1076-27871099-05262020-01-01202010.1155/2020/58751915875191Nonsingular Fast Terminal Adaptive Neuro-sliding Mode Control for Spacecraft Formation Flying SystemsXiaohan Lin0Xiaoping Shi1Shilun Li2Sing Kiong Nguang3Liruo Zhang4Control and Simulation Center, Harbin Institute of Technology, Harbin 150080, ChinaControl and Simulation Center, Harbin Institute of Technology, Harbin 150080, ChinaSchool of Astronautics, Harbin Institute of Technology, Harbin 150001, ChinaDepartment of Electrical, Computer and Software Engineering, The University of Auckland, Auckland 1142, New ZealandDepartment of Electrical, Computer and Software Engineering, The University of Auckland, Auckland 1142, New ZealandIn this paper, a nonsingular fast terminal adaptive neurosliding mode control for spacecraft formation flying systems is investigated. First, a supertwisting disturbance observer is employed to estimate external disturbances in the system. Second, a fast nonsingular terminal sliding mode control law is proposed to guarantee the tracking errors of the spacecraft formation converge to zero in finite time. Third, for the unknown parts in the spacecraft formation flying dynamics, we proposed an adaptive neurosliding mode control law to compensate them. The proposed sliding mode control laws not only achieve the formation but also alleviate the effect of the chattering. Finally, simulations are used to demonstrate the effectiveness of the proposed control laws.http://dx.doi.org/10.1155/2020/5875191
spellingShingle Xiaohan Lin
Xiaoping Shi
Shilun Li
Sing Kiong Nguang
Liruo Zhang
Nonsingular Fast Terminal Adaptive Neuro-sliding Mode Control for Spacecraft Formation Flying Systems
Complexity
title Nonsingular Fast Terminal Adaptive Neuro-sliding Mode Control for Spacecraft Formation Flying Systems
title_full Nonsingular Fast Terminal Adaptive Neuro-sliding Mode Control for Spacecraft Formation Flying Systems
title_fullStr Nonsingular Fast Terminal Adaptive Neuro-sliding Mode Control for Spacecraft Formation Flying Systems
title_full_unstemmed Nonsingular Fast Terminal Adaptive Neuro-sliding Mode Control for Spacecraft Formation Flying Systems
title_short Nonsingular Fast Terminal Adaptive Neuro-sliding Mode Control for Spacecraft Formation Flying Systems
title_sort nonsingular fast terminal adaptive neuro sliding mode control for spacecraft formation flying systems
url http://dx.doi.org/10.1155/2020/5875191
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AT xiaopingshi nonsingularfastterminaladaptiveneuroslidingmodecontrolforspacecraftformationflyingsystems
AT shilunli nonsingularfastterminaladaptiveneuroslidingmodecontrolforspacecraftformationflyingsystems
AT singkiongnguang nonsingularfastterminaladaptiveneuroslidingmodecontrolforspacecraftformationflyingsystems
AT liruozhang nonsingularfastterminaladaptiveneuroslidingmodecontrolforspacecraftformationflyingsystems