کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
765940 1462522 2012 9 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Inflatable Wing Design Parameter Optimization Using Orthogonal Testing and Support Vector Machines
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Inflatable Wing Design Parameter Optimization Using Orthogonal Testing and Support Vector Machines
چکیده انگلیسی

The robust parameter design method is a traditional approach to robust experimental design that seeks to obtain the optimal combination of factors/levels. To overcome some of the defects of the inflatable wing parameter design method, this paper proposes an optimization design scheme based on orthogonal testing and support vector machines (SVMs). Orthogonal testing design is used to estimate the appropriate initial value and variation domain of each variable to decrease the number of iterations and improve the identification accuracy and efficiency. Orthogonal tests consisting of three factors and three levels are designed to analyze the parameters of pressure, uniform applied load and the number of chambers that affect the bending response of inflatable wings. An SVM intelligent model is established and limited orthogonal test swatches are studied. Thus, the precise relationships between each parameter and product quality features, as well the signal-to-noise ratio (SNR), can be obtained. This can guide general technological design optimization.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Chinese Journal of Aeronautics - Volume 25, Issue 6, December 2012, Pages 887-895