Predetermined Performance Control of Spacecraft Formation Based on SE(3) Error Description

For the obstacle avoidance and formation maintenance issues of spacecraft formation, a control method with prescribed performance is proposed. Firstly, an error description system based on SE (3) is established. Secondly, to simplify the control system, collision avoidance, formation control of lead...

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Main Authors: Lijun Li, Yuanda Wang, Qin Yang, Erhan Wang
Format: Article
Language:English
Published: Wiley 2025-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/ijae/8765666
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author Lijun Li
Yuanda Wang
Qin Yang
Erhan Wang
author_facet Lijun Li
Yuanda Wang
Qin Yang
Erhan Wang
author_sort Lijun Li
collection DOAJ
description For the obstacle avoidance and formation maintenance issues of spacecraft formation, a control method with prescribed performance is proposed. Firstly, an error description system based on SE (3) is established. Secondly, to simplify the control system, collision avoidance, formation control of leading spacecraft, and containment control of following spacecraft are combined. Finally, the control errors are kept within the prescribed performance function range using prescribed performance control. Simulation results of spacecraft formation completing complex tasks under external disturbances validate the effectiveness of the proposed control scheme.
format Article
id doaj-art-c7bea3b01f28407f99f2dc9f62334ec8
institution Kabale University
issn 1687-5974
language English
publishDate 2025-01-01
publisher Wiley
record_format Article
series International Journal of Aerospace Engineering
spelling doaj-art-c7bea3b01f28407f99f2dc9f62334ec82025-02-08T00:00:04ZengWileyInternational Journal of Aerospace Engineering1687-59742025-01-01202510.1155/ijae/8765666Predetermined Performance Control of Spacecraft Formation Based on SE(3) Error DescriptionLijun Li0Yuanda Wang1Qin Yang2Erhan Wang3School of AutomationSchool of AutomationSchool of Mechanical EngineeringSchool of Mechanical EngineeringFor the obstacle avoidance and formation maintenance issues of spacecraft formation, a control method with prescribed performance is proposed. Firstly, an error description system based on SE (3) is established. Secondly, to simplify the control system, collision avoidance, formation control of leading spacecraft, and containment control of following spacecraft are combined. Finally, the control errors are kept within the prescribed performance function range using prescribed performance control. Simulation results of spacecraft formation completing complex tasks under external disturbances validate the effectiveness of the proposed control scheme.http://dx.doi.org/10.1155/ijae/8765666
spellingShingle Lijun Li
Yuanda Wang
Qin Yang
Erhan Wang
Predetermined Performance Control of Spacecraft Formation Based on SE(3) Error Description
International Journal of Aerospace Engineering
title Predetermined Performance Control of Spacecraft Formation Based on SE(3) Error Description
title_full Predetermined Performance Control of Spacecraft Formation Based on SE(3) Error Description
title_fullStr Predetermined Performance Control of Spacecraft Formation Based on SE(3) Error Description
title_full_unstemmed Predetermined Performance Control of Spacecraft Formation Based on SE(3) Error Description
title_short Predetermined Performance Control of Spacecraft Formation Based on SE(3) Error Description
title_sort predetermined performance control of spacecraft formation based on se 3 error description
url http://dx.doi.org/10.1155/ijae/8765666
work_keys_str_mv AT lijunli predeterminedperformancecontrolofspacecraftformationbasedonse3errordescription
AT yuandawang predeterminedperformancecontrolofspacecraftformationbasedonse3errordescription
AT qinyang predeterminedperformancecontrolofspacecraftformationbasedonse3errordescription
AT erhanwang predeterminedperformancecontrolofspacecraftformationbasedonse3errordescription