Attitude and Orbit Optimal Control of Combined Spacecraft via a Fully-Actuated System Approach
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Title
Attitude and Orbit Optimal Control of Combined Spacecraft via a Fully-Actuated System Approach
Authors
Keywords
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Journal
Journal of Systems Science & Complexity
Volume 35, Issue 2, Pages 623-640
Publisher
Springer Science and Business Media LLC
Online
2022-04-18
DOI
10.1007/s11424-022-1492-y
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