Enhanced attitude tracking control of spacecraft via inner and outer loop sliding mode design.

The significance of spacecraft in modern aerospace and technology is indisputable, with attitude control systems (ACS) playing a vital role in ensuring mission accuracy and safety. This study presents a dual-loop sliding mode variable structure control approach for spacecraft attitude regulation, le...

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Bibliographic Details
Main Authors: Xinxiang Fang, Ming Wen
Format: Article
Language:English
Published: Public Library of Science (PLoS) 2025-01-01
Series:PLoS ONE
Online Access:https://doi.org/10.1371/journal.pone.0328622
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