Closed-loop vibration control simulation of a helicopter active rotor with trailing-edge flaps based on the weighted-least-squares-error identification method

Closed-loop vibration control simulation of a helicopter active rotor with trailing-edge flaps based on the weighted-least-squares-error identification method

ZHOU Jinlong1,DONG Linghua1,YANG Weidong1,LIU Shiming2

Journal of Vibration and Shock ›› 2019, Vol. 38 ›› Issue (4) : 237-244.

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PDF(1479 KB)

Journal of Vibration and Shock ›› 2019, Vol. 38 ›› Issue (4) : 237-244.

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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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2019, 38(4): 237-244

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