DocumentCode
181497
Title
Automation of aircraft control reconfiguration in flight special situations
Author
Kazak, V.M. ; Vovk, V.G. ; Shevchuk, D.O. ; Levchenko, M.H.
Author_Institution
Dept. of Automatization & Powerenergy, Nat. Aviation Univ., Kiev, Ukraine
fYear
2014
fDate
14-17 Oct. 2014
Firstpage
161
Lastpage
164
Abstract
The paper explains the possibility of applying the system of parametric methods, structural reconfiguration control and reconfiguration of the object control objectives to prevent the transition to the current flight situation into a catastrophic one and maintain the specified level of safety. The article presents a block diagram of a control system developed reconfigurable dynamic system, and describes how it works.
Keywords
aircraft control; diagrams; aircraft control reconfiguration automation; block diagram; flight special situations; parametric method; structural reconfiguration control; Actuators; Aerospace control; Aircraft; Atmospheric modeling; Fault tolerance; Vectors; aircraft; faults or failures to the actuators/sensors or structural damage; flight control system; loss of control in flight; reconfiguration; survivability;
fLanguage
English
Publisher
ieee
Conference_Titel
Methods and Systems of Navigation and Motion Control (MSNMC), 2014 IEEE 3rd International Conference on
Conference_Location
Kiev
Print_ISBN
978-1-4799-6578-6
Type
conf
DOI
10.1109/MSNMC.2014.6979759
Filename
6979759
Link To Document