... ; 飞行器 ; 再入 ; 攻角设计 ; 法向过载动态平衡 [gap=1215]Key words: Sub-orbital; Vehicle; Re-entry; Attack angle design; normal acceleration dynamic equilibrium ..
基于1个网页-相关网页
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。
应用推荐