Automated identification system baseds on the changing of the temperature field of aircraft elements
| dc.contributor.author | Шевчук, Д.О. | uk_UA |
| dc.date.accessioned | 2019-04-11T10:05:35Z | |
| dc.date.available | 2019-04-11T10:05:35Z | |
| dc.date.issued | 2013 | |
| dc.description.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 | en |
| dc.identifier.issn | 1990-5548 | |
| dc.identifier.uri | http://er.nau.edu.ua/handle/NAU/38379 | |
| dc.language.iso | en | en |
| dc.publisher | National Aviation University | en |
| dc.subject | identification system | en |
| dc.subject | aircraft | en |
| dc.subject | structural damage | en |
| dc.subject | reconfiguration | en |
| dc.subject | flight control system | en |
| dc.subject | loss of control in flight | en |
| dc.subject | stability and controllability | en |
| dc.title | Automated identification system baseds on the changing of the temperature field of aircraft elements | en |
| dc.type | Article | en |