METHOD OF THE AIRCRAFT CONTROL RECONFIGURATION WHEN UNEXPECTED SITUATION APPEARS DURING FLIGHT
DOI:
https://doi.org/10.18372/2306-1472.59.6773Keywords:
aircraft, flight control system, loss-of-control, reconfiguration, stability and controllability, unexpected situationAbstract
Comparative analysis of the ICAO statistics showed that 35% of the aircraft losses associated with failures and damages of automatic control systems, mainly with failures of drives and external damage of tours and controllers. Classification of approaches to reconfigurable flight control systems is shown. The aim of this work is to develop method of reconfiguration to save the stability and controllability of the aircraft during the collisions with mechanical, biological and electrical elements.References
Access to the FAA National Wildlife Aircraft Strike Database and Associated ERAU Analytical/Statistical/Database Modules. Available from Internet: <http://wildlife.pr.erau.edu/ index.html>
Allan, J.R.; Orosz, A.P. The Costs of Birdstrikes to Commercial Aviation. Bird Strike Committee Proceedings, Bird Strike Committee USA/Canada, Third Joint Annual Meeting. Calgary, AB. 2001. 10 p.
Chingiz, H. Smart reconfigurable fault-tolerant flight control against actuator failures. International Federation of Automatic Control (IFAC). 2011. P. 3009-3011.
Cleary, E. Wildlife Strikes to Civil Aircraft in the United States 1990-2004. Federal Aviation Administration National Strike Database. 2005.
N 11. 77 p.
Hajiyev, Ch.; Caliskan, F. Integrated sensor/ actuator FDI and reconfigurable control for fault-tolerant flight control system design. The Aeronautical Journal. 2001. Vol. 105, N.1051. P. 525–533.
Halim, Alwi B. Eng. Fault tolerant sliding mode control schemes with aerospace applications. Leicester Control and Instrumentation Research Group Department of Engineering University of Leicester. 2006.
Kazak, V.M. System recovery methods survivability aircraft in special situations in flight. Monograph. Kyiv, National Aviation University “NAU-printing”. 2010. 284 p. (in Ukrainian).
Kulik, N.S.; Kharchenko, V.P.; Lutskiy, M.G. Encyclopedia of the safety flight. Kyiv, Tehnіka. 2008. 1000 p. (in Russian).
Liu, G.; Wang, D.; Li Y. Active fault tolerant control with actuation reconfiguration. IEEE Transactions on Aerospace and Electronic Systems. 2004. Vol. 40, N 3. P. 1110-1117.
Naryzhniy, A.G.; Pavlenko, V.N.; Svetlichny, S.P. Analysis of factors associated with cases of bird impact in the aircraft engine. Aerospace and Technology. 2011. N 6. P. 62 66 (in Russian).
Patton, R.J. Fault tolerant control: the 1997 situation. Proceedings of the IFAC Symposium SAFEPROCESS’97.Washington.1997.P.1035–1055.
Ryzhov, S.K. Aircrafts collision with birds. Airport partner. 2009. N 6. P. 30 32 (in Russian).
Shevchuk, D.O. Fiber-optic intelligence systems for diagnostics contraction integrity of aircrafts. Proceedings of the National Aviation University. 2010. N 1(42). P. 78–83.
Vishinskiy, V. Plane Collision with bird. Physical Elective. Quantum. 2009. N 6. P. 30–31. (in Russian).
Wu, N.E.; Zhang, Y.; Zhou, K. Detection, estimation, and accommodation of loss of control effectiveness. International Journal of Adaptive Control and Signal Processing. 2000. Vol. 14. P. 775–795.
Zhang, Y.; Jiang, J. (2002). Active fault tolerant control system against partial actuator failures. IEEE Proceedings Control Theory Application. 2002. Vol. 149, N 1. P. 95–104.
Zhao, Q.; Jiang, J. Reliable state feedback control system design against actuator failures. Automatica.1998. Vol. 34, N10. P. 1267–1272.
Allan, J.R.; Orosz, A.P. The Costs of Birdstrikes to Commercial Aviation. Bird Strike Committee Proceedings, Bird Strike Committee USA/Canada, Third Joint Annual Meeting. Calgary, AB. 2001. 10 p.
Chingiz, H. Smart reconfigurable fault-tolerant flight control against actuator failures. International Federation of Automatic Control (IFAC). 2011. P. 3009-3011.
Cleary, E. Wildlife Strikes to Civil Aircraft in the United States 1990-2004. Federal Aviation Administration National Strike Database. 2005.
N 11. 77 p.
Hajiyev, Ch.; Caliskan, F. Integrated sensor/ actuator FDI and reconfigurable control for fault-tolerant flight control system design. The Aeronautical Journal. 2001. Vol. 105, N.1051. P. 525–533.
Halim, Alwi B. Eng. Fault tolerant sliding mode control schemes with aerospace applications. Leicester Control and Instrumentation Research Group Department of Engineering University of Leicester. 2006.
Kazak, V.M. System recovery methods survivability aircraft in special situations in flight. Monograph. Kyiv, National Aviation University “NAU-printing”. 2010. 284 p. (in Ukrainian).
Kulik, N.S.; Kharchenko, V.P.; Lutskiy, M.G. Encyclopedia of the safety flight. Kyiv, Tehnіka. 2008. 1000 p. (in Russian).
Liu, G.; Wang, D.; Li Y. Active fault tolerant control with actuation reconfiguration. IEEE Transactions on Aerospace and Electronic Systems. 2004. Vol. 40, N 3. P. 1110-1117.
Naryzhniy, A.G.; Pavlenko, V.N.; Svetlichny, S.P. Analysis of factors associated with cases of bird impact in the aircraft engine. Aerospace and Technology. 2011. N 6. P. 62 66 (in Russian).
Patton, R.J. Fault tolerant control: the 1997 situation. Proceedings of the IFAC Symposium SAFEPROCESS’97.Washington.1997.P.1035–1055.
Ryzhov, S.K. Aircrafts collision with birds. Airport partner. 2009. N 6. P. 30 32 (in Russian).
Shevchuk, D.O. Fiber-optic intelligence systems for diagnostics contraction integrity of aircrafts. Proceedings of the National Aviation University. 2010. N 1(42). P. 78–83.
Vishinskiy, V. Plane Collision with bird. Physical Elective. Quantum. 2009. N 6. P. 30–31. (in Russian).
Wu, N.E.; Zhang, Y.; Zhou, K. Detection, estimation, and accommodation of loss of control effectiveness. International Journal of Adaptive Control and Signal Processing. 2000. Vol. 14. P. 775–795.
Zhang, Y.; Jiang, J. (2002). Active fault tolerant control system against partial actuator failures. IEEE Proceedings Control Theory Application. 2002. Vol. 149, N 1. P. 95–104.
Zhao, Q.; Jiang, J. Reliable state feedback control system design against actuator failures. Automatica.1998. Vol. 34, N10. P. 1267–1272.
Downloads
Published
04-07-2014
How to Cite
Shevchuk, D. (2014). METHOD OF THE AIRCRAFT CONTROL RECONFIGURATION WHEN UNEXPECTED SITUATION APPEARS DURING FLIGHT. Proceedings of National Aviation University, 59(2), 44–50. https://doi.org/10.18372/2306-1472.59.6773
Issue
Section
AEROSPACE SYSTEMS FOR MONITORING AND CONTROL
