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本文研究了弹性飞行器操纵机构最优位置的确定。在具有速率反馈的控制系统中,把控制作用看作等效阻尼,推导了由气动弹性效应所决定的舵面最优位置准则,给出了表征舵面位置与陀螺位置协调关系的公式。附有实例验证。
This paper studies the determination of the optimal position of the control mechanism of the flexible aircraft. In the control system with velocity feedback, the control effect is regarded as the equivalent damping. The optimal rudder position criterion derived from the aeroelastic effect is deduced. The formula that characterizes the coordination between rudder position and gyroscope position is given. With examples of validation.