Filter Observer-Based Attitude Control for Moving Mass Satellites Under Strong Aerodynamic Torques

Moving mass technology offers a promising solution to counter strong aerodynamic torques despite inherent inertial disturbance challenges. This paper proposes a filter observer-based attitude compensation scheme for low Earth orbit (LEO) moving mass satellites. The scheme integrates a moving mass de...

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Bibliographic Details
Main Authors: Yuandong Hu, Zhengliang Lu, Wenhe Liao
Format: Article
Language:English
Published: American Association for the Advancement of Science (AAAS) 2025-01-01
Series:Space: Science & Technology
Online Access:https://spj.science.org/doi/10.34133/space.0230
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