{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,6,20]],"date-time":"2026-06-20T09:31:38Z","timestamp":1781947898091,"version":"3.54.5"},"reference-count":47,"publisher":"American Institute of Aeronautics and Astronautics (AIAA)","issue":"10","funder":[{"name":"Canada Research Chair in Aircraft Modeling and Simulation"}],"content-domain":{"domain":["arc.aiaa.org"],"crossmark-restriction":true},"short-container-title":["Journal of Aerospace Information Systems"],"published-print":{"date-parts":[[2024,10]]},"abstract":"<jats:p> This paper presents a new control law based on type-2 fuzzy logic system (T2FLS) for the Cessna Citation X aircraft during cruise. This methodology combines three control systems: a T2FLS, a sliding mode control (SMC) system, and an adaptive control system. Differing from conventional controllers, this control system can deal with uncertainties and aircraft dynamics variations using the T2FLS approximator. The approximated functions were updated during the simulation iterations using adaptation laws derived from the Lyapunov theorem. The adaptability characteristic of this controller allows updating the approximated functions while the other design parameters remain unchanged. This fact simplifies the controller design process and eliminates the need to use a group of conventional controllers with different gains to control the aircraft in various flight conditions. In addition, the sliding mode control system helps to guarantee the aircraft\u2019s stability and robustness, along with two other methodologies in the presence and absence of turbulence. The performance of this control methodology was validated with a nonlinear simulation platform developed for the Cessna Citation X business aircraft using accurate flight data derived from a Level D flight simulator at the Research Laboratory in Active Controls, Avionics and AeroServoElasticity (LARCASE). <\/jats:p>","DOI":"10.2514\/1.i011398","type":"journal-article","created":{"date-parts":[[2024,9,12]],"date-time":"2024-09-12T11:53:31Z","timestamp":1726142011000},"page":"846-864","update-policy":"https:\/\/doi.org\/10.2514\/aiaa_crossmarkpolicy","source":"Crossref","is-referenced-by-count":3,"title":["New Type-2-Fuzzy-Logic-Based Control System for the Cessna Citation X"],"prefix":"10.2514","volume":"21","author":[{"given":"Seyed Mohammad","family":"Hosseini","sequence":"first","affiliation":[{"name":"\u00c9cole de Technologie Sup\u00e9rieure (\u00c9TS)"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Georges","family":"Ghazi","sequence":"additional","affiliation":[{"name":"\u00c9cole de Technologie Sup\u00e9rieure (\u00c9TS)"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0002-0911-6646","authenticated-orcid":false,"given":"Ruxandra Mihaela","family":"Botez","sequence":"additional","affiliation":[{"name":"\u00c9cole de Technologie Sup\u00e9rieure (\u00c9TS)"}],"role":[{"vocabulary":"crossref","role":"author"}]}],"member":"1387","reference":[{"key":"r1","doi-asserted-by":"publisher","DOI":"10.2514\/1.G007501"},{"issue":"4","key":"r2","first-page":"137","volume":"1","author":"Moncayo H.","year":"2013","journal-title":"Journal of Modeling, Simulation, Identification, and Control"},{"key":"r3","doi-asserted-by":"publisher","DOI":"10.1108\/IJIUS-03-2014-0002"},{"key":"r4","doi-asserted-by":"publisher","DOI":"10.2514\/1.G006173"},{"key":"r5","doi-asserted-by":"publisher","DOI":"10.1016\/j.conengprac.2021.104763"},{"key":"r6","doi-asserted-by":"publisher","DOI":"10.1016\/j.ifacol.2018.05.101"},{"key":"r7","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2019.105468"},{"key":"r9","doi-asserted-by":"publisher","DOI":"10.1016\/j.conengprac.2020.104721"},{"key":"r11","doi-asserted-by":"publisher","DOI":"10.3390\/s19010024"},{"key":"r12","doi-asserted-by":"publisher","DOI":"10.1016\/j.amc.2021.126053"},{"key":"r13","doi-asserted-by":"publisher","DOI":"10.22266\/ijies2017.0630.06"},{"key":"r14","doi-asserted-by":"publisher","DOI":"10.1109\/TCYB.2020.2987811"},{"key":"r16","doi-asserted-by":"publisher","DOI":"10.1002\/rnc.6577"},{"key":"r17","doi-asserted-by":"publisher","DOI":"10.1049\/iet-cta.2018.6262"},{"key":"r18","doi-asserted-by":"publisher","DOI":"10.1016\/j.isatra.2019.04.034"},{"issue":"4","key":"r19","doi-asserted-by":"crossref","first-page":"479","DOI":"10.18280\/jesa.530405","volume":"53","author":"Tavoosi J.","year":"2020","journal-title":"Journal Europ\u00e9en des Syst\u00e8mes Automatis\u00e9s"},{"key":"r20","doi-asserted-by":"publisher","DOI":"10.1109\/TFUZZ.2017.2773422"},{"key":"r21","doi-asserted-by":"publisher","DOI":"10.1115\/1.4030613"},{"key":"r22","doi-asserted-by":"publisher","DOI":"10.1016\/j.isatra.2015.09.006"},{"key":"r23","doi-asserted-by":"publisher","DOI":"10.1109\/TFUZZ.2021.3049902"},{"key":"r25","doi-asserted-by":"publisher","DOI":"10.1177\/0954410017712329"},{"key":"r28","doi-asserted-by":"publisher","DOI":"10.1177\/0954410016640821"},{"key":"r29","doi-asserted-by":"publisher","DOI":"10.13111\/2066-8201.2017.9.2.3"},{"key":"r30","doi-asserted-by":"publisher","DOI":"10.13111\/2066-8201.2017.9.2.4"},{"key":"r33","doi-asserted-by":"publisher","DOI":"10.1155\/2019\/7325053"},{"key":"r34","doi-asserted-by":"publisher","DOI":"10.3233\/IFS-141166"},{"key":"r35","doi-asserted-by":"publisher","DOI":"10.1002\/9781119174882"},{"key":"r36","volume-title":"Flight Dynamics and Control of Aero and Space Vehicles","author":"Yedavalli R. 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