Thesis Details
Automatic Flight Control System Design for a Jet Aircraft
This bachelor's thesis deals with the modelling of flight characteristics of a jet airplane and subsequent design and implementation of an automatic flight control system. Its goal was to implement a model of a jet airplane based on publicly available aerodynamic data of F-16 aircraft and use this model as a platform for the design and implementation of an automatic flight control system based on the non-linear dynamic inversion with a focus on controlling the pitch angle of an airplane by setting a desired value of the angle of attack. Conducted tests of the created system proved the ability of the control system to reach and maintain the desired angle of attack.
mathematical model of an airplane, flight control system, autopilot, non-linear dynamic inversion
Burget Lukáš, doc. Ing., Ph.D. (DCGM FIT BUT), člen
Kotásek Zdeněk, doc. Ing., CSc. (DCSY FIT BUT), člen
Křena Bohuslav, Ing., Ph.D. (DITS FIT BUT), člen
Matoušek Petr, doc. Ing., Ph.D., M.A. (DIFS FIT BUT), člen
@bachelorsthesis{FITBT17228, author = "Milan Kras\v{n}ansk\'{y}", type = "Bachelor's thesis", title = "Automatic Flight Control System Design for a Jet Aircraft", school = "Brno University of Technology, Faculty of Information Technology", year = 2015, location = "Brno, CZ", language = "english", url = "https://www.fit.vut.cz/study/thesis/17228/" }