Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/4058
Title: LQI Control Design with LQG Regulator via UKF for a Fixed-Wing Aircraft
Authors: Demirhan, E. N.
Çağlar Coşkun, K.
Kasnakoğlu, Coşku
Keywords: Fixed-Wing Aircraft
LQG Regulator
LQI Control
LQR
Unscented Kalman Filter
Issue Date: Oct-2020
Publisher: Institute of Electrical and Electronics Engineers Inc.
Source: Demirhan, 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.
Abstract: The 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.
URI: https://hdl.handle.net/20.500.11851/4058
https://ieeexplore.ieee.org/document/9259728
ISBN: 978-172819809-5
Appears in Collections:Elektrik ve Elektronik Mühendisliği Bölümü / Department of Electrical & Electronics Engineering
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
WoS İndeksli Yayınlar Koleksiyonu / WoS Indexed Publications Collection

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