In this paper, the method of reentry maneuver guidance applying to attack the ground fixed target is described by using flight dynamics principle and modern control theory.
本文运用飞行力学原理和现代控制理论，对攻击地面固定目标的飞行器的再入机动制导方法进行了研究。
In terms of the aircraft characteristics, the aircraft dynamics are divided into fast dynamics of Angle speeds and slow dynamics of roll Angle, Angle of attack and sideslip Angle.
根据飞机的动态特性，将飞机动态分为角速度快速动态与滚转角、迎角与侧滑角表示的慢动态。
Another nonlinear inversion controller was designed for the slow variables. It allows the pilot to control the slow dynamics, the Angle of attack, side-slip Angle and the velocity bank Angle.
对慢变量进行非线性逆控制器的设计可使飞行员控制飞机慢动力学，即迎角、侧滑角和速度矢量滚转角。
First, the simplified dynamics and kinematics model of attack helicopter air-combat are created, and the specific method on simplification of the model is given.
首先建立了简化的武装直升机空战动力学和运动学模型，阐明了模型简化的具体方法；
Milton Babbitt created his time point system, where the distance in time between attack points for the notes is serialized also, while some composers serialized aspects such as register or dynamics.
米尔顿·巴比特便据此创造了自己的时序系统，使得每个音符的起奏点之间的时间距离也呈现序列的关系。
When the Angle of attack is small or more than Angle of attack of buffeting, the shock control bump has little effect on the dynamics of airfoil.
而当迎角较小或超过抖振迎角后该激波控制鼓包不会对基本翼型的气动性能产生较大影响。
When the Angle of attack is small or when it is larger than the buffet onset Angle, the shock control bump has little effect on the dynamics of the airfoil.
而当迎角较小或超过抖振迎角后该激波控制鼓包不会对基本翼型的气动性能产生较大影响。
When the Angle of attack is small or when it is larger than the buffet onset Angle, the shock control bump has little effect on the dynamics of the airfoil.
而当迎角较小或超过抖振迎角后该激波控制鼓包不会对基本翼型的气动性能产生较大影响。
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