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基于多目标遗传算法的再入飞行器气动布局优化
Aerodynamic shape optimization of reentry body using Pareto genetic algorithm
【摘要】 本文采用多目标遗传算法来确定再入飞行器气动布局优化问题的Pareto最优解集 ,并和传统的多目标优化方法 (加权和方法、约束法 )进行比较。通过计算表明 ,多目标遗传算法能够在一次运行中搜索到优化问题的近似Pareto最优解集 ,这为飞行器设计者进行目标折衷决策提供了充分的依据。
【Abstract】 The Pareto genetic algorithm is modified to solve the engineering problems of the aerodynamic shape optimization of reentry body. The comparison of the traditional multi objective optimization methods with the Pareto genetic algorithm is also shown. The two design examples for crew transfer vehicle (CTV) and the maneuvering nose bent reentry body are provided. It is shown that the Pareto genetic algorithm may approximately provide the Pareto optimal set of the multi objective optimization problem, which is useful for designer to make compromise decision.
【关键词】 再入飞行器;
气动布局;
多目标优化;
多目标遗传算法;
【Key words】 reentry body; aerodynamic shape optimization; multi objective optimization; Pareto genetic algorithm;
【Key words】 reentry body; aerodynamic shape optimization; multi objective optimization; Pareto genetic algorithm;
【基金】 国家自然科学基金资助项目
- 【文献出处】 空气动力学学报 ,Acta Aerodynamica Sinica , 编辑部邮箱 ,2001年04期
- 【分类号】V211.3
- 【被引频次】20
- 【下载频次】327