{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,3,31]],"date-time":"2026-03-31T14:08:49Z","timestamp":1774966129630,"version":"3.50.1"},"reference-count":28,"publisher":"SAGE Publications","issue":"7","license":[{"start":{"date-parts":[[2017,4,6]],"date-time":"2017-04-06T00:00:00Z","timestamp":1491436800000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/journals.sagepub.com\/page\/policies\/text-and-data-mining-license"}],"funder":[{"DOI":"10.13039\/501100001809","name":"National Natural Science Foundation of China","doi-asserted-by":"crossref","award":["11572248"],"award-info":[{"award-number":["11572248"]}],"id":[{"id":"10.13039\/501100001809","id-type":"DOI","asserted-by":"crossref"}]},{"DOI":"10.13039\/501100001809","name":"National Natural Science Foundation of China","doi-asserted-by":"publisher","award":["51577121"],"award-info":[{"award-number":["51577121"]}],"id":[{"id":"10.13039\/501100001809","id-type":"DOI","asserted-by":"publisher"}]}],"content-domain":{"domain":["journals.sagepub.com"],"crossmark-restriction":true},"short-container-title":["Transactions of the Institute of Measurement and Control"],"published-print":{"date-parts":[[2018,4]]},"abstract":"<jats:p> This paper develops an attitude takeover control structure for post-capture non-cooperative targets with actuator nonlinearities and faults. In this paper, the contingent actuator gain faults, deviation faults and the undesirable non-symmetric dead-zone nonlinearities of the actuator are all under consideration. An effective robust adaptive fault tolerant attitude control method is synthesized such that the actuator nonlinearities and faults can be well handled. As a result, the accurate attitude stabilization and tracking are maintained. Moreover, an extended fault tolerant attitude control scheme that can work well in the presence of inaccurate measurement information is proposed. Based on a quadratic Lyapunov function, the proof of the convergence is completed. Simulation results demonstrate the effectiveness and advantages of the proposed method. <\/jats:p>","DOI":"10.1177\/0142331217696143","type":"journal-article","created":{"date-parts":[[2017,4,7]],"date-time":"2017-04-07T02:35:01Z","timestamp":1491532501000},"page":"2116-2128","update-policy":"https:\/\/doi.org\/10.1177\/sage-journals-update-policy","source":"Crossref","is-referenced-by-count":16,"title":["Robust adaptive fault tolerant attitude control for post-capture non-cooperative targets with actuator nonlinearities"],"prefix":"10.1177","volume":"40","author":[{"given":"Zheng","family":"Wang","sequence":"first","affiliation":[{"name":"National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi\u2019an, PR China"},{"name":"School of Astronautics, Northwestern Polytechnical University, Xi\u2019an, PR China"}]},{"given":"Jianping","family":"Yuan","sequence":"additional","affiliation":[{"name":"National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi\u2019an, PR China"},{"name":"School of Astronautics, Northwestern Polytechnical University, Xi\u2019an, PR China"}]},{"given":"Yong","family":"Shi","sequence":"additional","affiliation":[{"name":"Stevens Institute of Technology, USA"}]},{"given":"Dejia","family":"Che","sequence":"additional","affiliation":[{"name":"National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi\u2019an, PR China"},{"name":"School of Astronautics, Northwestern Polytechnical University, Xi\u2019an, PR China"}]}],"member":"179","published-online":{"date-parts":[[2017,4,6]]},"reference":[{"key":"bibr1-0142331217696143","doi-asserted-by":"publisher","DOI":"10.1016\/j.automatica.2007.10.034"},{"issue":"8","key":"bibr2-0142331217696143","first-page":"1","volume":"68","author":"Angel FA","year":"2014","journal-title":"Progress Aerospace Science"},{"key":"bibr3-0142331217696143","volume-title":"Proceedings of the IAF Global Exploration Conference, Paper GLEX-2012.11.1.7x12334, International Astronautical Federation","author":"Brophy JR","year":"2012"},{"key":"bibr4-0142331217696143","doi-asserted-by":"publisher","DOI":"10.2514\/1.31158"},{"key":"bibr5-0142331217696143","doi-asserted-by":"publisher","DOI":"10.1109\/7.892682"},{"key":"bibr6-0142331217696143","doi-asserted-by":"publisher","DOI":"10.2514\/1.G001341"},{"key":"bibr7-0142331217696143","doi-asserted-by":"publisher","DOI":"10.2514\/3.21798"},{"key":"bibr8-0142331217696143","doi-asserted-by":"publisher","DOI":"10.2514\/6.2009-1870"},{"key":"bibr9-0142331217696143","first-page":"14","volume":"8385","author":"Floresabad A","year":"2012","journal-title":"Proceedings of SPIE - The International Society for Optical Engineering"},{"key":"bibr10-0142331217696143","volume-title":"International Symposium on Artificial Intelligence, Robotics and Automation in Space","author":"Henshaw CG","year":"2014"},{"key":"bibr11-0142331217696143","doi-asserted-by":"publisher","DOI":"10.1017\/S0263574714000617"},{"key":"bibr12-0142331217696143","doi-asserted-by":"publisher","DOI":"10.2514\/1.G001309"},{"key":"bibr13-0142331217696143","volume-title":"Spacecraft Attitude Dynamics","author":"Hughes PC","year":"2004"},{"key":"bibr14-0142331217696143","doi-asserted-by":"publisher","DOI":"10.1016\/j.automatica.2006.09.022"},{"key":"bibr15-0142331217696143","doi-asserted-by":"publisher","DOI":"10.1109\/TFUZZ.2010.2058808"},{"key":"bibr16-0142331217696143","doi-asserted-by":"publisher","DOI":"10.2514\/2.4192"},{"key":"bibr17-0142331217696143","doi-asserted-by":"publisher","DOI":"10.1109\/9.400476"},{"key":"bibr18-0142331217696143","doi-asserted-by":"publisher","DOI":"10.1007\/978-1-4471-4396-3"},{"key":"bibr19-0142331217696143","volume-title":"Proc. 58th IAC \u2018International Astronautical Congress\u2019 (IAC-07-A6.3.05)","author":"Liou JC","year":"2007"},{"key":"bibr20-0142331217696143","doi-asserted-by":"publisher","DOI":"10.1016\/j.amc.2006.07.035"},{"key":"bibr21-0142331217696143","doi-asserted-by":"publisher","DOI":"10.1016\/j.actaastro.2009.01.041"},{"key":"bibr22-0142331217696143","doi-asserted-by":"publisher","DOI":"10.1007\/BF00348720"},{"key":"bibr23-0142331217696143","doi-asserted-by":"publisher","DOI":"10.2514\/1.43029"},{"key":"bibr24-0142331217696143","doi-asserted-by":"publisher","DOI":"10.1016\/j.actaastro.2013.06.028"},{"key":"bibr25-0142331217696143","doi-asserted-by":"crossref","unstructured":"Wang Z (2015) Adaptive smooth second-order sliding mode control method with application to missile guidance. 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