000005457 001__ 5457 000005457 005__ 20150429092416.0 000005457 037__ $$aTAZ-PFC-2010-398 000005457 041__ $$aeng 000005457 1001_ $$aCortés Concha, Gloria 000005457 24500 $$aDevelopment of an automatic flight control system 000005457 260__ $$aZaragoza$$bUniversidad de Zaragoza$$c2010 000005457 506__ $$aby-nc-sa$$bCreative Commons$$c3.0$$uhttp://creativecommons.org/licenses/by-nc-sa/3.0/ 000005457 500__ $$aTrabajo cargado por la Biblioteca Hypatia. Para contactar con el autor utilice 535653@celes.unizar.es 000005457 520__ $$aIn the aviation industry, aircraft manufactures are constantly striving to fully understand the essentials required to successfully design an AFCS, based on dynamic response of the aircraft in relation to atmospheric turbulence and structural flexibility. This report is about the analysis of the longitudinal and lateral dynamics stability of an aircraft, based on the data of CHARLIE. Applying Stability Augmentation System (SAS), Attitude and Flight Path Control System. Furthermore, to achieve the control system in a good response it was simulated using Matlab environment. 000005457 521__ $$aIngeniero Técnico Industrial (Esp. Electricidad) 000005457 540__ $$aDerechos regulados por licencia Creative Commons 000005457 700__ $$aZouaoui, Zoubir$$edir. 000005457 7102_ $$aUniversidad de Zaragoza$$bIngeniería Eléctrica$$cIngeniería Eléctrica 000005457 7202_ $$aMontañés Espinosa, Antonio$$eponente 000005457 830__ $$aEUITIZ 000005457 8560_ $$fhypatia@unizar.es 000005457 8564_ $$s1488649$$uhttps://zaguan.unizar.es/record/5457/files/TAZ-PFC-2010-398_ANE.pdf$$zAnexos (eng) 000005457 8564_ $$s5162984$$uhttps://zaguan.unizar.es/record/5457/files/TAZ-PFC-2010-398.pdf$$yMemoria (eng)$$zMemoria (eng) 000005457 909CO $$ooai:zaguan.unizar.es:5457$$pdriver$$pproyectos-fin-carrera 000005457 950__ $$a 000005457 980__ $$aTAZ$$bPFC$$cEUITIZ