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机译:基于模糊多目标遗传算法(MOGA)的液体推进剂发动机概念设计
Department of Space Systems Engineering, Faculty of Aerospace Engineering, K.N. Toosi University of Technology, Tehran, Islamic Republic of Iran;
Department of Space Systems Engineering, Faculty of Aerospace Engineering, K.N. Toosi University of Technology, Tehran, Islamic Republic of Iran,K.N.Toosi University of Technology, University Street, East Vafadar Blv., Tehran 1957975713, Islamic Republic of Iran;
Department of Space Systems Engineering, Faculty of Aerospace Engineering, K.N. Toosi University of Technology, Tehran, Islamic Republic of Iran;
Department of Space Systems Engineering, Faculty of Aerospace Engineering, K.N. Toosi University of Technology, Tehran, Islamic Republic of Iran;
Multi-objective; genetic algorithm; MOGA; fuzzy approach; liquid propellant engine (LPE);
机译:基于协同优化和进化算法的液体推进剂发动机设计
机译:一种多目标,多学科的设计优化方法,用于航天器双推进系统的概念设计
机译:基于卡尔曼滤波和故障因子法的开式循环液体火箭发动机故障检测与诊断算法
机译:多目标遗传算法(MOGA)在各种发动机速度下阀门定时设计优化的应用
机译:遗传算法方法用于航天器系统的概念设计,包括多目标优化和不确定性下的设计。
机译:一种基于自适应遗传算法优化返回传播神经网络的液体火箭发动机实时故障检测方法
机译:使用梯度算法初步设计和优化大规模夹紧液体火箭发动机涡轮送料系统开放循环的新方法