带传统线性控制器飞机在大迎角高机动飞行时敏捷性明显地减小,运动状态严重耦合更加重这一趋势,而此时操纵能力往往仍有剩余而却未能被利用。
The agility of aircraft with conventional linear flight controllers tends to drop rapidly under high angles of attack, and kinematic coupling of motions furtherly promotes the tendency.
带传统线性控制器飞机在大迎角高机动飞行时敏捷性明显地减小,运动状态严重耦合更加重这一趋势,而此时操纵能力往往仍有剩余而却未能被利用。
The agility of aircraft with conventional linear flight controllers tends to drop rapidly under high angles of attack, and kinematic coupling of motions furtherly promotes the tendency.
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