Decentralized attitude synchronization of spacecraft formations under complex communication topology

The attitude synchronizing of formation flying spacecrafts is an essential ingredient in almost all practical situations. However, thus far no control scheme was proposed for synchronizing the attitude of multiple spacecraft without a prescribed reference attitude in the presence of disturbance torq...

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Main Authors: Zhipeng Wang, Zhaowei Sun, Xiande Wu, Haichao Liang, Jianying Wang
Format: Article
Language:English
Published: SAGE Publishing 2016-08-01
Series:Advances in Mechanical Engineering
Online Access:https://doi.org/10.1177/1687814016660464
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spelling doaj-c0c2a59f49be42c4a87aea9ef6e6d8322020-11-25T03:20:35ZengSAGE PublishingAdvances in Mechanical Engineering1687-81402016-08-01810.1177/168781401666046410.1177_1687814016660464Decentralized attitude synchronization of spacecraft formations under complex communication topologyZhipeng Wang0Zhaowei Sun1Xiande Wu2Haichao Liang3Jianying Wang4Research Center of Satellite Technology, Harbin Institute of Technology, Harbin, ChinaResearch Center of Satellite Technology, Harbin Institute of Technology, Harbin, ChinaCollege of Aerospace and Civil Engineering, Harbin Engineering University, Harbin, ChinaBeijing Institute of Long March Vehicle, Beijing, ChinaScience and Technology on Space Physics Laboratory, Beijing, ChinaThe attitude synchronizing of formation flying spacecrafts is an essential ingredient in almost all practical situations. However, thus far no control scheme was proposed for synchronizing the attitude of multiple spacecraft without a prescribed reference attitude in the presence of disturbance torques and limited communication topology. A decentralized robust attitude control law is proposed in order to guarantee spacecraft attitude synchronization under external disturbances in the absence of a common reference attitude or any other hierarchy in the formation. The proposed controller is effective with a large range of communication topologies and is designed using the absolute angular velocity and attitude quaternion. The control scheme is robust against environmental disturbance torques. The convergence and stability of the proposed controller for the resulting closed-loop system are proven theoretically. Numerical simulations are included to validate the analytical results.https://doi.org/10.1177/1687814016660464
collection DOAJ
language English
format Article
sources DOAJ
author Zhipeng Wang
Zhaowei Sun
Xiande Wu
Haichao Liang
Jianying Wang
spellingShingle Zhipeng Wang
Zhaowei Sun
Xiande Wu
Haichao Liang
Jianying Wang
Decentralized attitude synchronization of spacecraft formations under complex communication topology
Advances in Mechanical Engineering
author_facet Zhipeng Wang
Zhaowei Sun
Xiande Wu
Haichao Liang
Jianying Wang
author_sort Zhipeng Wang
title Decentralized attitude synchronization of spacecraft formations under complex communication topology
title_short Decentralized attitude synchronization of spacecraft formations under complex communication topology
title_full Decentralized attitude synchronization of spacecraft formations under complex communication topology
title_fullStr Decentralized attitude synchronization of spacecraft formations under complex communication topology
title_full_unstemmed Decentralized attitude synchronization of spacecraft formations under complex communication topology
title_sort decentralized attitude synchronization of spacecraft formations under complex communication topology
publisher SAGE Publishing
series Advances in Mechanical Engineering
issn 1687-8140
publishDate 2016-08-01
description The attitude synchronizing of formation flying spacecrafts is an essential ingredient in almost all practical situations. However, thus far no control scheme was proposed for synchronizing the attitude of multiple spacecraft without a prescribed reference attitude in the presence of disturbance torques and limited communication topology. A decentralized robust attitude control law is proposed in order to guarantee spacecraft attitude synchronization under external disturbances in the absence of a common reference attitude or any other hierarchy in the formation. The proposed controller is effective with a large range of communication topologies and is designed using the absolute angular velocity and attitude quaternion. The control scheme is robust against environmental disturbance torques. The convergence and stability of the proposed controller for the resulting closed-loop system are proven theoretically. Numerical simulations are included to validate the analytical results.
url https://doi.org/10.1177/1687814016660464
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AT xiandewu decentralizedattitudesynchronizationofspacecraftformationsundercomplexcommunicationtopology
AT haichaoliang decentralizedattitudesynchronizationofspacecraftformationsundercomplexcommunicationtopology
AT jianyingwang decentralizedattitudesynchronizationofspacecraftformationsundercomplexcommunicationtopology
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