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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2016-08-01
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Series: | Advances in Mechanical Engineering |
Online Access: | https://doi.org/10.1177/1687814016660464 |
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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 |
work_keys_str_mv |
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