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dc.contributor.authorDemirhan, E.N.
dc.contributor.authorCaglar Coskun, K.
dc.contributor.authorKasnakoğlu, Coşku
dc.date.accessioned2021-01-25T11:32:57Z
dc.date.available2021-01-25T11:32:57Z
dc.date.issued2020-10
dc.identifier.citationDemirhan, E. N., Coşkun, K. Ç., and Kasnakoğlu, C. (2020, October). LQI Control Design with LQG Regulator via UKF for a Fixed-Wing Aircraft. In 2020 24th International Conference on System Theory, Control and Computing (ICSTCC) (pp. 25-30). IEEE.en_US
dc.identifier.isbn978-172819809-5
dc.identifier.urihttps://ieeexplore.ieee.org/document/9259728
dc.identifier.urihttp://hdl.handle.net/20.500.11851/4058
dc.description24th International Conference on System Theory, Control and Computing (2020 : Virtual, Sinaia; Romania)en_US
dc.description.abstractThe purpose of this work is designing a Linear Quadratic Gaussian (LQG) regulator and a Linear Quadratic Integral (LQI) controller for a fixed-wing aircraft. The LQG regulator design is created in two steps. First, an Unscented Kalman Filter (UKF) is selected as an observer for system dynamics to procreate an overall best estimate of system states. Second, an optimal feedback gain is calculated via the Linear Quadratic Regulator (LQR) approach. An LQI controller is designed for robust tracking of referenced outputs which are airspeed, sideslip, pitch angle and roll angle. The proposed LQG/LQI scheme is implemented in the MATLAB, Simulink environment. The simulation results show that the implemented system regulates and controls the system successfully in a noisy environment. © 2020 IEEE.en_US
dc.language.isoengen_US
dc.publisherInstitute of Electrical and Electronics Engineers Inc.en_US
dc.relation.ispartof2020 24th International Conference on System Theory, Control and Computing, ICSTCC 2020 - Proceedings
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectFixed-Wing Aircraften_US
dc.subjectLQG Regulatoren_US
dc.subjectLQI Controlen_US
dc.subjectLQRen_US
dc.subjectUnscented Kalman Filteren_US
dc.titleLQI Control Design with LQG Regulator via UKF for a Fixed-Wing Aircraften_US
dc.typeconferenceObjecten_US
dc.contributor.departmentTOBB ETU, Faculty of Engineering, Department of Electrical & Electronics Engineeringen_US
dc.contributor.departmentTOBB ETÜ, Mühendislik Fakültesi, Elektrik ve Elektronik Mühendisliği Bölümütr_TR
dc.identifier.startpage25
dc.identifier.endpage30
dc.contributor.orcidhttps://orcid.org/0000-0002-9928-727X
dc.identifier.scopus2-s2.0-85098006093
dc.contributor.tobbetuauthorKasnakoğlu, Coşku
dc.identifier.doi10.1109/ICSTCC50638.2020.9259728
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıtr_TR


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