๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

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

โœ Scribed by Hu, Qinglei


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

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


On-off attitude control of flexible sate
โœ Skaar, S. B. ;Tang, L. ;Yalda-Mooshabad, I. ๐Ÿ“‚ Article ๐Ÿ“… 1986 ๐Ÿ› American Institute of Aeronautics and Astronautics ๐ŸŒ English โš– 424 KB
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