DocumentCode
633640
Title
Sliding Mode Control of Electromagnetic Spacecraft Formation Flying in Near-Earth Orbits
Author
Shen, Ying ; Yuan, Changqing
fYear
2013
fDate
29-30 June 2013
Firstpage
1211
Lastpage
1213
Abstract
A sliding mode control for six-degree-of-freedom electromagnetic spacecraft formation flying (EMFF) in near-Earth orbits is presented. By using terminal sliding mode technique, the output tracking error can converge to zero in finite time, and strong robustness with respect to disturbance forces can be guaranteed. Illustrative simulations of EMFF are conducted to verify the effectiveness of the proposed controller.
Keywords
Near-Earth Orbits; Sliding Mode; electromagnetic spacecraft formation;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Manufacturing and Automation (ICDMA), 2013 Fourth International Conference on
Conference_Location
Shinan District of Qingdao ??Shangdong Province, China
Type
conf
DOI
10.1109/ICDMA.2013.287
Filename
6598211
Link To Document