DocumentCode :
48808
Title :
Corrections to “Finite-Time Attitude Tracking Control for Spacecraft Using Terminal Sliding Model and Chebyshev Neural Network”
Author :
Zou, An-Min ; Kumar, K. Deepak ; Hou, Zeng-Guang
Author_Institution :
Department of Aerospace Engineering, Ryerson University, Toronto, Canada
Volume :
43
Issue :
2
fYear :
2013
fDate :
Apr-13
Firstpage :
803
Lastpage :
803
Abstract :
Errors in the above-named article [ibid., vol. 41, no. 4, pp. 950-963, Aug. 2011] are noted for pages 952, 955, and 956.
Keywords :
Adaptive control; Artificial neural networks; Attitude control; Chebyshev approximation; Space vehicles;
fLanguage :
English
Journal_Title :
Cybernetics, IEEE Transactions on
Publisher :
ieee
ISSN :
2168-2267
Type :
jour
DOI :
10.1109/TSMCB.2012.2215317
Filename :
6316199
Link To Document :
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