A geometrical parameter optimization method of a longitudinally connected air suspension based on a second generation non-dominated genetic algorithm nested in an inner layer and an outer layer
A technology of geometric parameters and genetic algorithm, applied in the field of optimization of key geometric parameters of longitudinally connected air suspension, can solve the problems of lack of optimization of geometric parameters, increased cargo damage, increased ruts, cracks, loose pits and peeling, etc.
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[0065] In this embodiment, a method for optimizing the geometric parameters of the longitudinally connected air suspension based on the second-generation non-dominated genetic algorithm nested in the inner and outer layers is as follows: figure 1 As shown, it proceeds as follows:
[0066] Step 1. Establish a multi-objective optimization model for key geometric parameters of the longitudinally connected air suspension.
[0067] Step 1.1, for the structure of the longitudinally connected air suspension, such as figure 2 As shown, a three-axle semi-trailer-road coupling mathematical model is constructed; the vehicle model contains five degrees of freedom: the vertical displacement Z of the sprung mass, and the vertical displacement x of the three unsprung masses 1 、x 2 、x 3 , and the pitch angle of the sprung mass The equation of motion is as follows:
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[0073] In formula (1)-(5), m t1 ,m t2 ,m t3 and q 1 ,q2 ,...
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