DYNAMICS OF NON-AUTONOMOUS SPATIAL MOTION OF AN AEROPLANE WITH DEFORMABLE CONTROL SYSTEMS.

被引：0
|
作者：
Dzygadlo, Z.
Krzyzanowski, A.
机构：
来源：
Journal of Technical Physics | 1984年 / 25卷 / 01期
关键词：
EQUATIONS OF MOTION - MATHEMATICAL TECHNIQUES - Numerical Analysis;
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摘要：
The aeroplane is a spatial object acted on, during flight, by various forces due to the recoil of aircraft guns, rocket firing, bomb dropping etc. The influence of the external forces on the dynamics of spatial motion of the aircraft has been studied assuming constant coefficients of stiffness and damping in the control systems. The influence of the stiffness and damping in the controls has been analyzed by numerical means. This has been completed by a resonance analysis of the oscillation of the control surfaces and its influence on the dynamics of spatial motion of the aircraft.
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页码：53 / 78
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