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 |
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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