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Simultaneous Vibration Reduction and Attitude Control of Flexible Spacecraft with On-Off Actuators

✍ Scribed by Hu, Qinglei

Book ID: 120004264
Publisher: TSI Press
Year: 2011
Tongue: English
Weight: 355 KB
Volume: 17
Category: Article
ISSN: 1079-8587
DOI: 10.1080/10798587.2011.10643153

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## Abstract After publication, it was determined that this paper contained an error where Equation (36) cannot be solved because it is constrained by the inequality of Equation (30). To overcome this, we here change the mistake into a static output feedback problem. Equation (29) can be rewritten