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Optimal spacecraft terminal attitude control synthesis by the quaternion method

✍ Scribed by M. V. Levskii

Book ID: 111494353
Publisher: Allerton Press Inc
Year: 2009
Tongue: English
Weight: 692 KB
Volume: 44
Category: Article
ISSN: 0025-6544
DOI: 10.3103/s0025654409020022

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