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Inverse multi-step prediction model method for MIMO random vibration test control
ZHENG Wei, CHEN Huaihai
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2020, (2): 223000 -223000 .  DOI: 10.7527/S1000-6893.2019.23000

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341