In order to attack the target with big impact Angle, over compensation of gravity is added to the design.
为了实现大落角攻击目标，进行了末制导过重补设计。
The extended linearization of nonlinear systems is used to design flight control systems at high angle of attack.
利用非线性系统的扩展线性化方法设计具有大迎角的非线性飞行控制系统。
This kinetic model can be used in ballistic calculation of projectile with large angle of attack and also in the design of some smart munitions(e. g. target sensitivity projectile).
此动力学模型可用于弹丸大攻角飞行时的弹道计算及某些灵巧弹药（如末敏弹）的设计。
The paper has introduced design of the support system for rotary balance of high attack angle, and the importance and methods of studying spin of aircraft.
为此，设计了大攻角旋转天平支撑系统，此系统可测定飞机模型在不同姿态角下绕风轴以一系列恒定的角速率旋转时的气动特性。
The optimization of maximum attack Angle is evaluated according to the given initial design parameters by using the orthogonal method.
最大攻角的优化根据给定的初始设计值采用正交法进行。
The optimization of maximum attack Angle is evaluated according to the given initial design parameters by using the orthogonal method.
最大攻角的优化根据给定的初始设计值采用正交法进行。
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