Technical Stability of Dynamic States of Controlled Elastic Aircraft

被引：0
|
作者：
K. S. Matviichuk
机构：
[1] National Academy of Sciences of Ukraine,S. P. Timoshenko Institute of Mechanics
来源：
International Applied Mechanics | 2001年 / 37卷
关键词：
Dynamic Process; Dynamic State; Vertical Motion; Positive Parameter; Aerodynamic Force;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Sufficient conditions are obtained for the technical stability of the controlled longitudinal vertical motion of elongated elastic aircraft. These aircraft are considered to have a variable cross-section and to be subject to significant transverse deformations and vibrations. The technical-stability criteria formulated depend on a small positive parameter. This parameter is a function of key parameters of the controlled dynamic process such as the increment in the transverse load due to the curvature of the system axis and the aerodynamic forces
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页码：550 / 563
页数：13
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