自适应现状制导律

Adaptive actuality boost guidance law

针对反弹道导弹的导弹武器的主动飞行段,提出了高精度自适应现状制导律。通过实时修正飞行程序,以消除导弹飞行过程中遇到的各种干扰的影响,保证命中精度,并对发动机推力偏差、风干扰影响下的导弹运动进行了数学仿真,仿真结果证实了自适应现状制导律是合理、可行的。

A new adaptive actuality guidance law is presented for the boost phase of anti-ballistic missile weapons.In order to ensure intercepting precision,this guidance law is used to correct the flight programming for washing away the influence of interference in flight process of missile.Computer simulation for the movement of interceptor under influence of wind and thrust divergence shows that the guidance law is reasonable and feasible.