Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/3889
Title: Control Loss Recovery Autopilot Design for Fixed-Wing Aircraft
Authors: Akyürek, Şeyma
Kürkçü, Burak
Kaynak, Ünver
Kasnakoğlu, Coşku
Keywords: Loop-shaping
power loss
numerical simulation
loss of control
autopilot design
Issue Date: 2016
Publisher: Elsevier B.V.
Source: Akyürek, Ş., Kürkçü, B., Kaynak, Ü., & Kasnakoğlu, C. (2016). Control loss recovery autopilot design for fixed-wing aircraft. IFAC-PapersOnLine, 49(9), 117-123.
Abstract: In this paper a loop-shaping design approach is investigated for distressed fixed-wing aircraft experiencing control loss due to surface or power failure. An accurate nonlinear model of the aircraft dynamics is utilized to obtain a target aircraft behavior in the emergency situation, for which a loop-shaping controller is designed to balance performance and robustness, and to decouple different command channels. A rudder servoactuator jam scenario is presented as an example where it is seen that the autopilot recovers level flight and responds well to fly-by-wire commands from the operator.
Description: 6th IFAC Symposium on System Structure and Control (SSSC) (2016: Istanbul)
URI: https://www.sciencedirect.com/science/article/pii/S2405896316307236?via%3Dihub
https://hdl.handle.net/20.500.11851/3889
ISSN: 24058963
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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