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First, an active fault detection scheme is proposed by designing a nonlinear fault detection observer for the faulty hypersonic flight vehicle model. A finite-time convergence fault-tolerant controller is proposed on the basis of combined back-stepping and sliding mode technology. Moreover, the adaptive law is developed to estimate the bound information of actuator efficiency factor. The fault-free controller is accomplished which guarantees the globally asymptotic output tracking and boundedness of the closed-loop system. Finally, numerical simulations in Simulation and Verification Platform are presented to illustrate that the proposed fault-tolerant control strategy is effective in providing satisfactory tracking performance and rejecting actuator faults in a climbing maneuver case.<\/jats:p>","DOI":"10.1177\/0959651814552809","type":"journal-article","created":{"date-parts":[[2014,10,29]],"date-time":"2014-10-29T01:45:50Z","timestamp":1414547150000},"page":"130-138","update-policy":"https:\/\/doi.org\/10.1177\/sage-journals-update-policy","source":"Crossref","is-referenced-by-count":7,"title":["Adaptive active fault-tolerant control of generic hypersonic flight vehicles"],"prefix":"10.1177","volume":"229","author":[{"given":"Yuehui","family":"Ji","sequence":"first","affiliation":[{"name":"School of Electrical Engineering, and Tianjin Key Laboratory for Control Theory & Applications in Complicated Systems, Tianjin University of Technology, Tianjin City, 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