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Paper Publications
.Reducing Helicopter Vibration Loads by Individual Blade Control with Genetic Algorithm:Machines,2022,10(6)
.Fuzzy Neural Network PID Control Used in Individual Blade Control:Aerospace,2023,10(7)
.The Overall Design of Variable Diameter Ducted Fan in the Aircraft:Aerospace,2022,9(7)
.Impact Load Identification Algorithm of Helicopter Weapon Pylon Based on Time-Domain Response Signal.[J]:Aerospace,2022,9(7)
Gao Yadong,Gao Yadong,徐永勤,李清龙.基于小波变换和神经网络的直升机旋翼不平衡故障诊断方法:南京航空航天大学学报,2017
Gao Yadong,Gao Yadong,顾景轶,李清龙,WANG Huaming.独立桨叶变距对旋翼振动载荷影响规律分析:南京航空航天大学学报,2018
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