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.[点击复制] |
Deng Jianhua.Non-Linear Maximum Likelihood -Optimization Method for Identifying Non-Linear Curve[J].Control Theory and Technology,1991,8(4):407~413.[点击复制] |
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辨识非线性曲线的非线性极大似然—优化法 |
Non-Linear Maximum Likelihood -Optimization Method for Identifying Non-Linear Curve |
摘要点击 1119 全文点击 468 投稿时间:1990-03-23 修订日期:1991-03-25 |
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DOI编号 |
1991,8(4):407-413 |
中文关键词 非线性曲线辨识 极大似然法 优化法 样条函数 飞行器极曲线 |
英文关键词 non-linear curve identification maximum likelihood method optimization method spline function polar curve of an aircraft |
基金项目 |
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中文摘要 |
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。 |
英文摘要 |
In the engineering field we are often faced with a problem that from test date is determined a non-linear curve which is strongly non-linear and not expressed by an analytical formula, e.g. it is absolutely necessary in aircraft flight test data analysis that from flight test data is determined a polar diagram (curve) which is a basic aerodynamic characteristics curve to calculate a flight performance. The above problem may be included in non-linear curve identification. In this paper research on a non-linear maximum likelihood-optimization method for identifying 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 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 (e.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 identity above polar curve of an aircraft are presented. |