基于响应面法的印制电路板组件有限元模型修正  

Finite element model updating of printed circuit board assembly based on response surface methodology

作　　者：王开山 李传日[1] 庞月婵 郭恒晖 

机构地区：[1]北京航空航天大学可靠性与系统工程学院,北京100191

出　　处：《振动与冲击》2015年第22期42-46,共5页Journal of Vibration and Shock

摘　　要：在将印制电路板及元器件材料视为正交各向异性前提下,提出基于响应面法的印制电路板组件(Printed Circuit Board Assembly,PCBA)有限元模型修正法。利用相关性分析筛选出对PCBA模态频率影响较大参数作为修正参数;据修正参数数目选择合适的试验设计获取样本点,构造多项式响应面模型;通过最小二乘法确定多项式系数并检验响应面拟合精度;用响应面计算结果与模态试验结果误差绝对值构造目标函数;通过多目标遗传算法(MOGA)迭代计算获得优化修正参数并代入有限元模型获得修正模型。以某航空电子产品某PCBA为案例,对比修正前后各阶模态频率与试验值误差。结果表明,修正后模型各阶模态频率与试验值相对误差均明显减小,验证该方法对PCBA模型修正的有效性。On the premise of taking the materials of the printed circuit board and its components as orthotropic, a method based on response surface was proposed to update the finite element model （FEM） of printed circuit board assembly（PCBA）.The parameters which have great influence on the modal frequencies of PCBA were screened out and taken as the updating parameters by correlation analysis.The sample points were acquired by using an appropriate experimental design according to the number of the updating parameters to construct a polynomial response surface model. The least squares method was used to determine the polynomial coefficients and then to test the fitting accuracy of response surface.The absolute value of error between the result of the calculated response surface and that of an actual test was taken as an objective function.The optimized parameters were obtained taking advantage of the iterative calculation of the multiple objectives genetic algorithm （MOGA ）.The updated model was then obtained by substituting the optimized parameters into the non-updated FEM.Taking the PCBA of an aircraft electronic product as an example,the comparison between the modal frequencies of non-updated and updated FEM shows that the relative error of modal frequencies of the updated FEM to the actual test is obviously reduced and thus verifies the effectiveness of the model updating methodology suggested.

关 键 词：各向异性 印制电路板组件 模型修正 相关性分析 响应面法 优化求解 

分 类 号：V414[航空宇航科学与技术—航空宇航推进理论与工程] TB330[一般工业技术—材料科学与工程]