首页 | 本学科首页   官方微博 | 高级检索  
     

辨识非线性曲线的非线性极大似然—优化法
引用本文:邓建华. 辨识非线性曲线的非线性极大似然—优化法[J]. 控制理论与应用, 1991, 8(4): 407-413
作者姓名:邓建华
作者单位:西北工业大学飞机系 西安
摘    要:工程上经常碰到非线性曲线辨识问题。本文探讨一种非线性极大似然-优化法并结合三次样条函数拟配法,形成统一的逐次逼近的直接辨识非线性曲线的非线性辨识方法。该法兼有极大似然法的唯一性、很好的收敛性和优化法直接处理非线性系统的能力,辨识出的样条函数曲线能无限地光滑地逼近非线性曲线。

关 键 词:非线性 曲线 极大似然 最佳化
收稿时间:1990-03-23
修稿时间:1991-03-25

Non-Linear Maximum Likelihood -Optimization Method for Identifying Non-Linear Curve
Deng Jianhua. Non-Linear Maximum Likelihood -Optimization Method for Identifying Non-Linear Curve[J]. Control Theory & Applications, 1991, 8(4): 407-413
Authors:Deng Jianhua
Affiliation:Department of Aircraft Engineering, Northwestern Polytechnical University
Abstract:In the engineering field we arc often faced with a problem that from test data is determined a non-linear curve which is strongly non-linear and not expressed by an analytical formula ,c. g. it is absolutely necessaryin aircraft flight test data analysis that from flight test data is determined a polar diagram (curve) which is a basic aerodynamic characteristic curve to calculate a flight performance. The above problem may be included in non-lincar curve identification. In this paper research on a non-linear maximum likelihood-optimization method for identifying the non-linear curve is presented. A general idea of this method is : first the non-linear curve is approached by a suitable function system(e. g. a cubical spline-polynomial);secondly the non-linear curve identification is transformed into a normal parameter identification; thirdly a criterion of a maximum likelihood function is built; finally is established a unified successive iterate procedure that a criterion of the maximum likelihood function is driven into an extreme using an optimization method. This method has a uniqueness and a good astringency of the maximum likelihood method and a capability of solving a non-linear problem by the optimization method. An identified function curve (c. g. a cubical spline function curve) can approach the non-linear curve unlimitedly smoothly. In this paper a fundamental principle of this method and its application to identify above polar curve of an aircraft are presented.
Keywords:non-linear curve identification  maximum likelihood method  optimization method  spline function  polar curve of an aircraft
本文献已被 CNKI 维普 等数据库收录!
点击此处可从《控制理论与应用》浏览原始摘要信息
点击此处可从《控制理论与应用》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号