摘要
文中对无人机总体参数的多目标优化方法进行了研究,并利用线性加权和法将总体参数的多目标优化问题转化为单目标优化问题进行求解,在此基础上建立了喷气式无人机总体设计模型和相应的计算机多目标优化设计算法及程序。通过在某无人机总体方案设计中的应用,验证了该方法的合理性和有效性。
This paper has discussed the method for multi-objective optimization of UAV configuration parameter at first. As for the multi-objective optimization problem, it is turned to single-objective optimization by using weighting objectives method. Then the relevant computer programs for multi-objective optimization of UAV configuration parameter have be written. The method has been successfully used in the configuration design of our UAV and validated its rationality and validity.
出处
《弹箭与制导学报》
CSCD
北大核心
2006年第3期340-342,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
无人机
总体参数
多目标优化
UAV
configuration parameter
multi-objective optimization