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SIMULATION OF AIRCRAFT ABRUPT RESPONSE IN DIRECTIONAL CONTROL

卷 41, 册 4, 2010, pp. 471-480
DOI: 10.1615/TsAGISciJ.v41.i4.80
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摘要

Considered are the problems of on-ground, motion-on simulation of specific forces and angular accelerations arising from aircraft abrupt response (AR) to pilot activity with regard to directional control. A method to simulate specific forces and angular accelerations is developed to predict the AR phenomenon at the first stages of aircraft development. Special attention was paid to the selection of motion system drive algorithms and their parameters with regard to directional AR reproduction. The motion system drive algorithm parameters were selected for different piloting tasks.

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