DAMPING OF OSCILLATIONS IN FLIGHT CONTROL CIRCUITS OF SCHOOL AND TRAINING AIRCRAFT
The specific developments of Dutch roll mode have shown a number of flight dynamics deficiencies, prevailing in aircraft with fixed (non-assisted) controls in which the damping factor is at level 2.The project deals with the lateral motion damping (damper of gyration) issue according to the flight r...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2010-03-01
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Series: | INCAS Bulletin |
Online Access: | http://bulletin.incas.ro/files/bogdan_dobrescu_v2no1_full.pdf |