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Adaptive output feedback sliding-mode manoeuvring and vibration control of flexible spacecraft with input saturation

โœ Scribed by Hu, Q.


Book ID
117811448
Publisher
The Institution of Engineering and Technology
Year
2008
Tongue
English
Weight
616 KB
Volume
2
Category
Article
ISSN
1751-8644

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Manoeuvring and vibration reduction of a
โœ Qinglei Hu; Guangfu Ma ๐Ÿ“‚ Article ๐Ÿ“… 2007 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 37 KB ๐Ÿ‘ 1 views

## 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