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

Issue

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

DOI

10.1109/TSMCB.2012.2215317

Filename

6316199

Link To Document