基于非线性状态空间辨识的气动弹性模型降阶
1)
张家铭,杨执钧,黄锐
REDUCED-ORDER MODELING FOR AEROELASTIC SYSTEMS VIA NONLINEAR STATE-SPACE IDENTIFICATION
1)
Zhang Jiaming,Yang Zhijun,Huang Rui
表 1
BACT机翼结构参数
Table 1
Structural parameters of BACT wing