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采用系统拓扑优化的思路,通过最优化理论,把需要解决的设计问题简化为数学模型进行求解,在多个限制条件下寻求满足目标函数的最优解,获得了实现重量、变形、频率等约束下的飞行器结构设计优化结果。
According to the idea of system topology optimization, the design problem to be solved is simplified to a mathematical model by optimization theory, and the optimal solution to the objective function is sought under a variety of constraints. The constraints of weight, deformation, frequency, etc. are obtained Under the aircraft structure design optimization results.