UAV aircraft model for control system failures analysis

• Autorzy: Żugaj M. , Bibik P. , Jacewicz M.

Identyfikatory

DOI

10.15632/jtam-pl.54.4.1405

• Języki publikacji: EN

Abstrakty

EN

In the paper, influence of control surface failures on UAV aircraft dynamics is investigated. A method for control loads determination for a nonlinear UAV aircraft model is presented. The model has been developed to analyse the influence of various control surface failures on aircraft controllability and to form the background for developing reconfiguration methods of flight control systems. The analysis of the control system failure impact on the aircraft dynamics and the ability of the control system to reconfiguration are presented.

Słowa kluczowe

EN

UAV; flight dynamics; control; reconfiguration

• Wydawca: Polskie Towarzystwo Mechaniki Teoretycznej i Stosowanej
• Czasopismo: Journal of Theoretical and Applied Mechanics
• Rocznik: 2016
• Tom: Vol. 54 nr 4
• Strony: 1405--1415
• Opis fizyczny: Bibliogr. 17 poz., rys.

Twórcy

autor

Żugaj M.

• Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics, Warszawa, Poland

autor

Bibik P.

• Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics, Warszawa, Poland

autor

Jacewicz M.

• Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics, Warszawa, Poland

Bibliografia

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• 6. Kozak V.M., Shevchuk D.O., Vovk V.G., Levchenko M.H., 2014, Automation of aircraft control reconfiguration in flight special situations, Proceedings of IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control, 161-164
• 7. Lin X., Fulton N.L., Horn M.E.T., 2014, Quantification of high level safety criteria for civil unmanned aircraft systems, Proceedings of Aerospace Conference, Big Sky, 1-13
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• 11. Nizioł J., 2005, Dynamics of Mechanical Systems (in Polish), Komitet Mechaniki PAN, Instytut Podstawowych Problemów Techniki Polskiej Akademii Nauk, Warszawa
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• 14. Young A.D., 1953, The Aerodynamics Characteristics Of Flaps, A.R.C. Technical Report No. 2622 (10766), Her Majesty’s Stationery Office
• 15. Żugaj M., Narkiewicz J., 2007, Impact of control system degradation on aircraft flight performance (in Polish), Zeszyty Naukowe Politechniki Rzeszowskiej, Mechanika, 71, 179-186
• 16. Żugaj M., Narkiewicz J., 2009, Autopilot for reconfigurable flight control system, ASCE Journal of Aerospace Engineering, 22, 1, 78-84
• 17. Żugaj M., Narkiewicz J., 2010, Autopilot supported by nonlinear model following reconfigurable flight control system, ASCE Journal of Aerospace Engineering, 22, 1, 339-347

Uwagi

PL

Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniajacą naukę.