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为确定火箭弹射座椅动力稳定调节方法设计所应依据的人体参数,对292例飞行员的人体参数及人椅系统组合重心数据进行了回归分析研究,综合确定了以体重和身高作为调节依据参数,并求出了该参数与人椅系统组合重心的回归方程。研究结果已用于火箭弹射座椅动力稳定调节方法的设计研究中。
In order to determine the body parameters of the rocket ejection seat dynamic stability adjustment method design, the regression analysis of the body parameters of 292 pilots and the combined center of gravity data of the chair and chair system was conducted. The body weight and height were taken as the parameters for adjustment. And obtained the regression equation between the parameters and the center of gravity of the human-chair system. The research results have been used in the design and research of the dynamic stability regulation of rocket ejector seat.