The effectiveness of aero control decreases as dynamic pressure decreases. Therefore impulse attitude control motor(ACM) is to be used to maintain fast response of missile in low dynamic pressure.
气动控制在低动压时其效率会有相当下降,为了使导弹在低动压时仍然具有一定的快速响应性,在导弹上安装脉冲姿控发动机参与姿态控制是一条可行的途径。
The improvement of fire control system is an important method to heighten the efficiency of aero-weapons system.
航空火力控制系统的改进是提升飞机武器系统作战效能的一个重要手段。
In the matter - in - loop simulation experiment of aero - engine control system, the turbine outlet temperature, which characteristics with high and quick change , is hard to be simulated.
航空发动机控制系统半物理模拟试验中,涡轮出口气体温度高、变化快,难以模拟。
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