This paper introduces the research and application of flight dynamics in design of control augmentation system.
介绍了飞行力学在某型飞机控制增稳系统设计中的研究和应用.
On the basis of a250-seat BWB configuration, the control surfaces were first configured according to trim, stability augmentation and maneuverability considerations with margin for disturbances.
本文在一架250座级翼身融合客机布局设计基础上,根据平衡、增稳、机动等要求,设计了操纵面配置方案;
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