Please use this identifier to cite or link to this item:
|Title:||LQI Control Design with LQG Regulator via UKF for a Fixed-Wing Aircraft||Authors:||Demirhan, E. N.
Çağlar Coşkun, K.
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
|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
Show full item record
checked on Dec 26, 2022
Items in GCRIS Repository are protected by copyright, with all rights reserved, unless otherwise indicated.