Application of isocline plots of non-linear systems for aircraft stability under dynamic states

被引：0

作者：

Itaketo, U.T. ^{[1
]}

Ogbogu, S.O.E. ^{[1
]}

Chukwudebe, G.A. ^{[1
]}

机构：

[1] Federal Univ of Technology, Owerri, Nigeria

来源：

Advances in Modeling and Analysis C | 2000年 / 55卷 / 1-2期

关键词：

Aircraft - Aircraft engines - Aviators - Closed loop control systems - Cockpits (aircraft) - Flight dynamics - Gyroscopes - Natural frequencies - Oscillations - Position control - System stability;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

The concept of stability is defined. Conventional methods in determining the stability of non-linear systems are mentioned. One of those conventional methods, the method of isoclines, is illustrated but it has a shortcoming, which is mentioned. A method, developed by the authors, captioned: the modified isocline method, corrects that deficiency and is presented. How the developed method could be applied in real-life; for aircraft stability, is highlighted. It makes the isocline method and its trajectory plot a concise and complete procedure for determining the stability of non-linear systems. It is significant contribution to the advancement of control engineering by the authors.

引用

页码：53 / 64

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