The invention discloses a wing structure dynamics uncertainty solving method based on a symplectic characteristic line method, and belongs to the technical field of
structural dynamics uncertainty analysis. The method comprises the following steps: firstly, establishing a
cantilever beam model of a wing structure, determining uncertain parameters, and constructing a generalized probability
density evolution equation; selecting a representative sample point according to the parameter probability distribution and calculating an assigned probability; thirdly, converting a structural kinetic equation into a Hamiltonian
system form, and gradually solving a characteristic line by utilizing a characteristic line method of a hyperbolic equation and combining a symplectic
algorithm; and translating the initial condition along the feature line to obtain the probability
density distribution of each sample point, and finally superposing all sample point results to obtain a probability density function of the
system response. According to the method, the feature line solving precision is improved by introducing the symplectic
algorithm, the characteristics of the Hamiltonian
system are better maintained, and the precision of dynamic
uncertainty analysis of the wing structure is effectively improved.