TY - JOUR
T1 - 利用时延神经网络的动载荷倒序识别
AU - Xia, Peng
AU - Yang, Te
AU - Xu, Jiang
AU - Wang, Le
AU - Yang, Zhichun
N1 - Publisher Copyright:
© 2021, Beihang University Aerospace Knowledge Press. All right reserved.
PY - 2021/7/25
Y1 - 2021/7/25
N2 - The time delay neural network, extensively applied in speech recognition, is introduced to identify random dynamic loads. Combining the "memory" property of the time delay neural network with the causal Finite-Impulse-Response (FIR) system theory and the steady response solution of the vibration theory, we propose a reversed time sequence dynamic load identification method. Experimental verification of the proposed method is conducted using an aircraft rudder model excited by two-point random loads. The results demonstrate that the root mean square errors between the time histories of the identified and real dynamic load samples on the two loading points are 0.635 4 and 2.543 7, respectively, and the correlation coefficients are 0.9657 and 0.8262, respectively. The curve of the power spectral density function between the identified and real dynamic loads on the two loading points coincides fairly well. The proposed dynamic load identification method has the advantage of high precision and requires no structural modelling.
AB - The time delay neural network, extensively applied in speech recognition, is introduced to identify random dynamic loads. Combining the "memory" property of the time delay neural network with the causal Finite-Impulse-Response (FIR) system theory and the steady response solution of the vibration theory, we propose a reversed time sequence dynamic load identification method. Experimental verification of the proposed method is conducted using an aircraft rudder model excited by two-point random loads. The results demonstrate that the root mean square errors between the time histories of the identified and real dynamic load samples on the two loading points are 0.635 4 and 2.543 7, respectively, and the correlation coefficients are 0.9657 and 0.8262, respectively. The curve of the power spectral density function between the identified and real dynamic loads on the two loading points coincides fairly well. The proposed dynamic load identification method has the advantage of high precision and requires no structural modelling.
KW - Causal finite-impulse-response systems
KW - Load identification
KW - Random dynamic loads
KW - Reversed time sequence identification
KW - Time delay neural networks
UR - http://www.scopus.com/inward/record.url?scp=85111543949&partnerID=8YFLogxK
U2 - 10.7527/S1000-6893.2020.24452
DO - 10.7527/S1000-6893.2020.24452
M3 - 文章
AN - SCOPUS:85111543949
SN - 1000-6893
VL - 42
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 7
M1 - 224452
ER -