给定导弹目标线角速度的制导方法

The Guiding Method of Given Missile-target Line Angular Velocity

结合现有航空导弹制导方法的不足 ,介绍了一种国外导弹给定目标线角速度的新制导方法 ,并建立了数学模型 .模拟结果表明 。

Based on the analyzing the defect in the aero missile guiding method, a new guiding method given the missile target line angular velocity is introduced, and the mathematical model is proposed. The simulation result shows that the guiding method can rationally solve the contradicatory problem between the complication of missile guiding system and guiding precision.