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应用对策理论的多目标气动优化设计
引用本文:唐智礼.应用对策理论的多目标气动优化设计[J].南京航空航天大学学报(英文版),2005,22(3):195-199.
作者姓名:唐智礼
作者单位:南京航空航天大学航空宇航学院,中国南京210016
基金项目:国家自然科学基金(10372040)资助项目;国家教委留学回国科研启动基金(2003-091)资助项目;南京航空航天大学青年基金资助项目.
摘    要:将经济学中的Nash均衡理论引入到气动优化设计中,探索一种新颖的处理互为冲突的多目标气动外形优化设计方法.基本的优化器为基于伴随方法的确定性优化算法,文中通过引入负反馈技术发展了约束最优控制理论,所有的约束条件都被自动的和隐含的满足.在对称Nash策略中,每一个优化器都力图优化自己的目标,而Nash平衡则提供了多个目标之间的一种妥协解.设计算例表明,文中的Nash竞争策略在多目标气动优化设计中是有效的.

关 键 词:博弈理论  多目标优化  气动设计  约束最优控制理论
收稿时间:04 25 2005 12:00AM
修稿时间:06 20 2005 12:00AM

MULTI-OBJECTIVE SHAPE DESIGN IN AERODYNAMICS USING GAME STRATEGY
TANG Zhi-li.MULTI-OBJECTIVE SHAPE DESIGN IN AERODYNAMICS USING GAME STRATEGY[J].Transactions of Nanjing University of Aeronautics & Astronautics,2005,22(3):195-199.
Authors:TANG Zhi-li
Institution:College of Aerospace Engineering, NUAA, 29 Yudao Street, Nanjing,210016,P. R. China
Abstract:Multi-objective optimization for the optimum shape design is introduced in aerodynamics using the Game theory. Based on the control theory, the employed optimizer and the negative feedback are used to implement the constraints. All the constraints are satisfied implicitly and automatically in the design. Furthermore,the above methodology is combined with a formulation derived from the Game theory to treat multi-point airfoil optimization. Airfoil shapes are optimized according to various aerodynamics criteria. In the symmetric Nash game, each "player" is responsible for one criterion, and the Nash equilibrium provides a solution to the multipoint optimization. Design results confirm the efficiency of the method.
Keywords:Game theory  multi-objective optimization  aerodynamic design  constrained optimal control theory
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