Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/2832
Title: Altitude Control for Small Fixed-Wing Aircraft Using H-infinity Loop-Shaping Method
Authors: Akyürek, Şeyma
Kaynak, Ünver
Kasnakoğlu, Coşku
Keywords: Aircraft control
altitude control
automatic control
flight control
Loop-shaping control
stabilization
Issue Date: 2016
Publisher: Elsevier Science BV
Source: Akyurek, S., Kaynak, U., and Kasnakoglu, C. (2016). Altitude control for small fixed-wing aircraft using H? loop-shaping method. IFAC-PapersOnLine, 49(9), 111-116.
Abstract: Autopilot systems for UAVs without human pilots maintain the flight through an appropriate balance of aerodynamic forces autonomously. That is to say, they arc used to make flight missions more reliable and efficient. Autopilot system design architecture conventionally contains two sections, inner and outer loops. Inner loop is the stabilizer and the outer loop can provide one of the additional motion controls (or all) such as speed, altitude, and heading hold. In this paper, H-infinity Loop-shaping method is used to provide the stabilizer mode and the PID controller is used to control the altitude. (C) 2016, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.
URI: https://hdl.handle.net/20.500.11851/2832
https://www.sciencedirect.com/science/article/pii/S2405896316307212
ISSN: 2405-8963
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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