Structural Dynamics Optimization Design Method for A Spaceborne Radar
In response to the structural dynamics optimization design requirements of a certain satellite-borne precipitation ra-dar,based on finite element analysis,the Kriging surrogate model is used to approximate the finite element model of the satellite-borne precipitation radar.The improved genetic algorithm is then employed to optimize the honeycomb panel structure parameters,resulting in a better design solution.Finally,the effectiveness of this method is demonstrated through a case study of the structural dynamics optimization design of a certain satellite-borne precipitation radar and mechanical experiments.
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