Multidisciplinary Design Optimization of Torpedo General Design Based on Collaborative Optimization
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摘要: 为了使用多学科设计优化方法解决鱼雷总体设计中的并行设计、耦合变量等难题,提高鱼雷总体性能,该文提出了以最大航程为目标函数,对涉及到的航程、外形、推进器及能供学科进行多学科分析,并利用基于协同优化算法的多学科设计优化方法对鱼雷外形及推进器进行设计优化。仿真结果表明,该方法能够提高鱼雷航程。Abstract: In order to solve the problems such as coupled state variable and parallel design in torpedo general design using the method of multidisciplinary design optimization(MDO), we take the maximum range as objective function, and comprehensively analyse torpedo ′s range, shape,propulsion and fuel supply system. The collaborative optimization (CO) algorithm is adopted to optimize the design of shape and propeller.Simulation results show that the proposed optimization method can prolong torpedo range.
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[1] 王振国,陈小前,罗文彩,等.飞行器多学科设计优化理论与应用研究[M].北京:国防工业出版社,2006. [2] Kroo I.Multidisciplinary Optimization Methods for Aircraft Preliminary Design[R].AIAA-94-4325,1994. [3] Braun R D.Kroo I M.Development and Application of the Collaborative Optimization Architecture in a Multidisciplinary Design Environment[J].Multidisciplinary Design Optimization: State of the Art,SIAM,1997, 37(12): 58-59. [4] Braun R D,Moore A A,Kroo I M.Collaborative Architecture for Launch Vehicle Design[J].Journal of Spacecraft and Rockets,1997,34(4):478-486. [5] 张宇文.鱼雷外形设计[M].西安:西北工业大学出版社,1998.
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