To investigate the rolling control characteristics of canard-controlledmissile with fixed-tail, a numerical simulation method based on N-S formulation was conducted.
采用以N-S方程为主控方程的数值模拟方法,进行固定尾翼鸭式气动布局导弹的气动特性和流场数值模拟。
2
An effective method was proposed to deal with delay compensation time of self-oscillation linear actuator for a gun launched missilecontrolled with single channel.
针对某单通道控制炮射导弹所采用的自激振荡线性化舵机,给出了一种有效的舵机延迟补偿时间处理方法。
3
Optical fiber winding was a important technique in optical fiber guided missile, and lag Angle controlled by lead screw subsystem was a key factor in optical fiber precise winding.