An Improved Acoustic Model Identifying Method in Propeller Synchrophasing Control
Propeller synchrophasing control is an effective method to reduce cabin noise level of multiple propeller driven airplanes.An improved acoustic model identifying method using a mixed conjugate gradient method was proposed and validated by experiments.The influence of different data acquisition conditions on the identification accuracy was also studied.It is concluded that the improved method can improve the identification accuracy while reducing the real-time communication requirement between modules.
Propeller Synchrophasing Control Active Noise Control Acoustic Model Identifying
Yangyang Wang Xianghua Huang Tianhong Zhang Jiayi Shu Xiangcheng Zhao
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
国际会议
南京
英文
1-5
2013-08-20(万方平台首次上网日期,不代表论文的发表时间)