Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/2833
Title: Design of a Flight Stabilizer for Fixed-Wing Aircrafts Using H-infinity Loop Shaping Method
Authors: Akyürek, Şeyma
Ozden, Gizem Sezin
Kürkcü, Burak
Kaynak, Ünver
Kasnakoğlu, Coşku
Keywords: UAV
aircraft
drone
stabilizer
autopilot
control
loop shaping
H-infinity
Issue Date: 2015
Publisher: IEEE
Source: Akyurek, S., Ozden, G. S., Kurkcu, B., Kaynak, U., and Kasnakoglu, C. (2015, November). Design of a flight stabilizer for fixed-wing aircrafts using H? loop shaping method. In 2015 9th International Conference on Electrical and Electronics Engineering (ELECO) (pp. 790-795). IEEE.
Abstract: Autopilot systems for unmanned aerial vehicles (UAVs) and aircrafts provide flight missions without need of human input and make them more reliable and efficient. The first step of designing an autopilot is a stabilizer mode. Conventional autopilot systems have inner and outer loops. Stabilizer is the inner loop for an autopilot. In this paper designing an aircraft control system ensures good performance and robustness that allows control of roll, pitch and yaw angles will be declared. Aircraft dynamics are used to design the model of the control system in the MATLAB Simulink environment. Using loop shaping method to achieve stable and robust control system will be the strategy. Generated controllers to find the most effective one are embedded in the X-plane which is one of the realistic simulations.
URI: https://hdl.handle.net/20.500.11851/2833
https://ieeexplore.ieee.org/abstract/document/7394579
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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