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
收藏
页码：53 / 64
相关论文
共 50 条
12345