机翼非水平机动攻击方式研究

Study on Non-Horizontal Wing Maneuver Attack Mode

研究了飞机在低空高速转弯时机翼非水平机动攻击方式,包括目标相对运动学、火控解算原理、机动轨迹控制等,并建立火控解算模型。数字仿真表明,该火控解算模型是合理可行的,火力/飞行耦合器所生成的飞行操纵指令能够帮助驾驶员实现自动瞄准攻击的目的。

This paper studies the attack mode in case of non-horizontal wing maneuver during the turning of AC at a high speed in low altitude,including the target relative kinetics,fire control solution principle,maneuver trajectory control and so on,and also establishes the fire control solution model.The mathematical simulation shows that this fire control model is reasonable and feasible,and the flight control command generated from the fire/flight coupler is able to help the pilot realize the aim of automatic alignment attack.