Nonlinear System Identification of Folding Fins with Freeplay Using Direct Parameter Estimation

被引:12
|
作者
Ma, Zhi-Sai [1 ,2 ]
Wang, Bo [3 ]
Zhang, Xin [4 ]
Ding, Qian [1 ,2 ]
机构
[1] Tianjin Univ, Sch Mech Engn, Tianjin 300350, Peoples R China
[2] Tianjin Key Lab Nonlinear Dynam & Control, Tianjin 300350, Peoples R China
[3] Beijing Inst Struct & Environm Engn, Beijing 100076, Peoples R China
[4] Beijing Inst Elect Syst Engn, Beijing 100854, Peoples R China
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
AEROELASTIC ANALYSIS; AIRFOIL;
D O I
10.1155/2019/3978260
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Folding fins are widely adopted in missiles for the efficient use of space during storage and transportation, while nonlinear behavior of freeplay is inevitable due to the factors such as mismachining tolerance, assembly error, and abrasion. The problem of nonlinear system identification of folding fins with freeplay is considered in this paper. A direct parameter estimation method which can identify the nonlinear system with freeplay under base excitation is proposed and subsequently applied to establish the nonlinear dynamic model of a folding fin. The best set of coefficients is selected by using the significance test, allowing the proposed method to detect and locate the most relevant nonlinearities of the practical structure. Experimental results demonstrate that the proposed method is able to decouple the linear and nonlinear dynamics of a nonlinear structure and estimate natural frequencies of the derived linear system along with nonlinear internal forces in one computational step, even if no a priori knowledge of the type of nonlinearities is given.
引用
收藏
页数:8
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