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