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Particularly, the actuator is locked in-place and does not respond to subsequent commands. A multiple model scheme is proposed to detect and isolate the faults. In the multiple model scheme, a series of parallel observers are constructed, each of which is based on a model that describes the system in the presence of a particular actuator fault. In addition, quantum information technique is used to choose which model matches the current system. Furthermore, to estimate the locked position, a robust fast adaptive fault estimation algorithm based on linear matrix inequality technique is proposed by considering the disturbances. Finally, the simulation results show the efficiency of this scheme.<\/jats:p>","DOI":"10.1177\/0959651813511240","type":"journal-article","created":{"date-parts":[[2013,12,6]],"date-time":"2013-12-06T22:25:45Z","timestamp":1386368745000},"page":"182-190","update-policy":"https:\/\/doi.org\/10.1177\/sage-journals-update-policy","source":"Crossref","is-referenced-by-count":3,"title":["Multiple model\u2013based fault detection and diagnosis for helicopter with actuator faults via quantum information technique"],"prefix":"10.1177","volume":"228","author":[{"given":"Fuyang","family":"Chen","sequence":"first","affiliation":[{"name":"College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, P.R. China"}],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Shijun","family":"Zhang","sequence":"additional","affiliation":[{"name":"College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, P.R. 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