Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/2829
Title: Rudder Loss Recovery Autopilot System for a Small Fixed-Wing Aircraft
Authors: Akyürek, Şeyma
Güneş, Uygar
Elbir, Övunç
Kasnakoğlu, Coşku
Kaynak, Ünver
Keywords: Helicopters
aircraft control
small-scale unmanned
Issue Date: 2017
Publisher: IEEE
Source: Akyurek, S., Gunes, U., Elbir, O., Kasnakoglu, C., and Kaynak, U. (2017). Rudder loss recovery autopilot system for a small fixed-wing aircraft. In 2017 10th International Conference on Electrical and Electronics Engineering (ELECO) (pp. 752-757). IEEE.
Abstract: This paper presents an integrated way of development of an aircraft dynamic modeling including stability and control derivatives and ensuing autopilot design. Stability derivatives are calculated via an automated procedure using a spreadsheet method that is consistent with the MATLAB/Simulink block of the subject aircraft. Bifilar pendulum experiment is used to obtain the actual moment of inertias of the aircraft. The loop shaping control approach is implemented for the stabilizer mode of the subject autopilot system to decouple different command channels of the MIMO system. The system is built in MATLAB/Simulink environment.
URI: https://hdl.handle.net/20.500.11851/2829
https://ieeexplore.ieee.org/abstract/document/8266332
ISBN: 978-1-5386-1723-6
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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