Automated identification system baseds on the changing of the temperature field of aircraft elements
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Date
2013
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Publisher
National Aviation University
Abstract
In this article, system of identification collisions (structural damage) in the air, based on the change of the temperature field was given. Identification system provides information about type and size of aircraft damage to all systems during recovering the controllability of the aircraft when an unexpected problem occurs during a flight is proposed
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Keywords
identification system, aircraft, structural damage, reconfiguration, flight control system, loss of control in flight, stability and controllability