@article{ref1,
title="Flight Control System Damage Simulation Using Freely Flying Models",
journal="Aeronautical journal",
year="2005",
author="Sadovnychiy, S and Ryzhenko, A and Betin, A",
volume="109",
number="1091",
pages="45-50",
abstract="This article deals with a damage simulation of flight control systems during a flight. As a subject of flight tests the model of a classic aerodynamic aircraft scheme is considered. This aircraft has highly swept wings a moderate wing elongation and all-moving horizontal tail surfaces. The diagrams of flight parameters from flight tests of the freely flying models with loss of a control surface in flight are given. The investigation results for the failures leading to a sharp drop in the stiffness of the control units in the pitch channel are given. The damage investigation in horizontal flight and in complex manoeuvres is given.   <p>Language: en</p>",
language="en",
issn="0001-9240",
doi="",
url="http://dx.doi.org/"
}