PDF(1479 KB)
PDF(1479 KB)
PDF(1479 KB)
基于加权最小二乘法辨识的后缘襟翼智能旋翼振动载荷闭环控制仿真研究
({{custom_author.role_cn}}), {{javascript:window.custom_author_cn_index++;}}Closed-loop vibration control simulation of a helicopter active rotor with trailing-edge flaps based on the weighted-least-squares-error identification method
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