Continuous structure dynamic load interval identification method
A technology of dynamic load and identification method, applied in the aerospace field, can solve problems such as monotony, and achieve the effect of strong generalization ability, low requirements, and low storage requirements
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Embodiment 1
[0094] The aircraft body structure can be simplified as a continuous beam structure, and the finite element model of the continuous beam structure is as follows: figure 2 As shown, the geometric dimensions and material parameters of the continuous beam are shown in Table 1, where the density and elastic modulus are regarded as interval uncertain parameters. The continuous beam structure is divided into 10 Euler beam elements with a total of 11 nodes, and each node has 3 directional degrees of freedom. The first node of the continuous beam structure is fixed, and a vertical dynamic load is applied to the 6th and 11th nodes respectively, and the expressions are f 1 (t)=80000sin(10πt), f 2 (t)=20000sin(6πt)+30000sin(8πt), the load identification process is 1s, and the response measurement frequency is 1000Hz. Sampling is carried out in the space of 1.5 times the interval uncertainty domain, that is, the sampling interval of density is [6630,8970]kg / m 3 , the sampling interval...
Embodiment 2
[0098] The wing and rudder structure of the aircraft can be simplified as a continuous plate structure, and the finite element model of the continuous plate structure is as follows: Figure 4 shown. Among them, the density and elastic modulus are regarded as interval uncertain parameters, and the interval uncertainty domains are [850,1150] kg / m 3 and [178.5, 241.5] GPa. The continuous plate structure is divided into 12 units with a total of 20 nodes, and each node has 6 directional degrees of freedom. The first to fifth nodes of the continuous beam structure are fixed, and a vertical dynamic load is applied to the 13th node. The expressions are f(t)=900000sin(6πt)+500000sin(10πt), and the load identification process is 2s, the response measurement frequency is 1000Hz. The sampling interval of density uncertain variable is [800,1200]kg / m 3 , the sampling interval of the elastic modulus uncertain variable is [168,252]GPa. The sampling size of the Latin hypercube is 200, and...
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