Aiming at the dynamic monitoring requirements of wing skin deformation

a skin deformation reconstruction method based on inverse finite element method and strain information was studied. Firstly

the three-node triangular element was used to discretize the structure

and the Kirchhoff plate and shell bending theory was used to construct the mechanical model. Then

the relationship between strain and displacement is deduced theoretically

the reconstruction algorithm is constructed

and a visualization software platform is developed to display the deformation of wing skin structure in real time. Finally

the airfoil skin structure and square skin structure are taken as the research objects

and the correctness and versatility of the reconstruction algorithm are verified by simulation analysi

s. The results show that the root mean square error of structural deformation reconstruction is 1.2% and the reconstruction time is less than 20ms when the density of strain measuring points is 2/m

2

. The deformation reconstruction method based on the inverse finite element method can be used in the deformation reconstruction of wing skin

which has a promising application in the field of aircraft structural deformation monitoring.