Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/5592
Title: Automatic recovery and autonomous navigation of disabled aircraft after control surface actuator jam
Authors: Kasnakoğlu, Coşku
Kaynak, Ünver
Issue Date: 2010
Source: AIAA Guidance, Navigation, and Control Conference, 2 August 2010 through 5 August 2010, Toronto, ON, 93435
Abstract: Loss of flight control authority in result of a system damage or an actuator jam is known or suspected to be the potential cause of many aviation accidents. After losing one or several control surface actuators, sustaining the flight for a safe return home depends on the capability of the remaining surfaces' control authority and the engine power. In this study, automatic recovery and autonomous guidance of a disabled general aviation aircraft is demonstrated. A nonlinear aircraft model and a MATLAB/SIMULINK based flight dynamics and control toolboxes are used to develop flight control laws for the disabled aircraft. The flight control laws are first validated for steady trimmed flight conditions and an actuator jam is applied to demonstrate the automatic recovery and autonomous navigation of the aircraft. The autopilot is designed to handle different control actuator malfunctions including rudder or aileron jams. Different scenario based simulations show that the new autopilot design is capable of sustaining safe flight and autonomous navigation under such malfunctions. Copyright © 2010 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
URI: https://doi.org/10.2514/6.2010-7546
https://hdl.handle.net/20.500.11851/5592
ISBN: 9781600869624
Appears in Collections:Elektrik ve Elektronik Mühendisliği Bölümü / Department of Electrical & Electronics Engineering
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection

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