Attitude Control Systems is a subsystem within spacecraft engineering that governs the orientation of a small satellite in three-dimensional space by measuring and adjusting its angular position and rates relative to a reference frame, distinguishing it from other spacecraft subsystems through its specialized function in maintaining desired pointing accuracy and stability for mission operations.
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Harbin Institute of Technology
Harbin, China
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Beijing, China
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Beijing Institute of Technology
Beijing, China
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Northwestern Polytechnical University
Xi'an, China
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Toronto Metropolitan University
Toronto, Canada
29 h-index
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Nanjing University of Aeronautics and Astronautics
Nanjing, China
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Concordia University
Montreal, Canada
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Nanyang Technological University
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- Aerospace Science and Technology
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- Acta Astronautica
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- IEEE Transactions on Aerospace and Electronic Systems
97 publications · 5.1K citations
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- IEEE Transactions on Automatic Control
40 publications · 5K citations
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