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In this approach, the attitude error dynamics and the kinematics of the flexible spacecraft are first established. Then, a nonsingular terminal sliding-mode surface is designed, based on finite-time control theory. Applying the Chebyshev neural network, the uncertain dynamics induced by external disturbances and uncertain inertia parameters are approximated and estimated. The nominal control law and the compensation control law to obtain the active reconfiguration fault-tolerant controller are finally developed in normal and fault conditions, respectively. The closed-loop tracking system is proved to be uniformly ultimately bounded stable after a finite time. Numerical simulations are presented for a flexible spacecraft to illustrate the efficiency of the proposed controller.<\/jats:p>","DOI":"10.1177\/0142331218803410","type":"journal-article","created":{"date-parts":[[2018,11,27]],"date-time":"2018-11-27T13:15:06Z","timestamp":1543324506000},"page":"925-933","update-policy":"https:\/\/doi.org\/10.1177\/sage-journals-update-policy","source":"Crossref","is-referenced-by-count":18,"title":["Active attitude fault-tolerant tracking control of flexible spacecraft via the Chebyshev neural network"],"prefix":"10.1177","volume":"41","author":[{"given":"Kunfeng","family":"Lu","sequence":"first","affiliation":[{"name":"Beijing Aerospace Automatic Control Institute, China"},{"name":"Beijing Aerospace Automatic Control Institute, China; National Key Laboratory of Science and Technology on Aerospace Intelligent Control, China"}]},{"given":"Tianya","family":"Li","sequence":"additional","affiliation":[{"name":"Beijing Aerospace Automatic Control Institute, China"},{"name":"Beijing Aerospace Automatic Control Institute, China; National Key Laboratory of Science and Technology on Aerospace Intelligent Control, China"}]},{"given":"Lijun","family":"Zhang","sequence":"additional","affiliation":[{"name":"School of Automation, Beijing Institute of Technology, China"}]}],"member":"179","published-online":{"date-parts":[[2018,11,27]]},"reference":[{"key":"e_1_3_2_2_1","doi-asserted-by":"publisher","DOI":"10.1177\/1687814017690341."},{"key":"e_1_3_2_3_1","doi-asserted-by":"publisher","DOI":"10.1109\/TIE.2015.2455053"},{"key":"e_1_3_2_4_1","doi-asserted-by":"publisher","DOI":"10.1016\/j.actaastro.2015.11.004"},{"key":"e_1_3_2_5_1","doi-asserted-by":"publisher","DOI":"10.1016\/j.actaastro.2009.04.004"},{"key":"e_1_3_2_6_1","doi-asserted-by":"publisher","DOI":"10.1109\/TFUZZ.2016.2612264"},{"key":"e_1_3_2_7_1","doi-asserted-by":"publisher","DOI":"10.2514\/1.G000921"},{"key":"e_1_3_2_8_1","doi-asserted-by":"publisher","DOI":"10.1080\/00207721.2012.702236"},{"key":"e_1_3_2_9_1","doi-asserted-by":"publisher","DOI":"10.1049\/iet-cta.2009.0628"},{"key":"e_1_3_2_10_1","doi-asserted-by":"publisher","DOI":"10.1109\/TSMC.2016.2564918"},{"key":"e_1_3_2_11_1","doi-asserted-by":"publisher","DOI":"10.1016\/j.ijnonlinmec.2009.12.008"},{"key":"e_1_3_2_12_1","doi-asserted-by":"publisher","DOI":"10.1016\/j.automatica.2014.10.095"},{"key":"e_1_3_2_13_1","doi-asserted-by":"publisher","DOI":"10.1109\/CDC.2011.6161267"},{"key":"e_1_3_2_14_1","first-page":"532","article-title":"Sampled-data control of spacecraft rendezvous with discontinuous Lyapunov approach","volume":"6","author":"Li Z","year":"2013","unstructured":"Li Z, Liu M, Karimi H, et al. 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