基于运动耦合的战术导弹协调控制技术

Tactical Missile's Coordinate Control Technology Based on Movement Coupling

为进一步提升战术导弹机动转弯过程中的协调度,满足新一代战术导弹冲压发动机进气对侧滑角约束需求,研究了基于运动耦合的协调控制技术。结合经典的过载控制方案,重点研究了以三通道运动耦合为基础的抑制侧滑角控制技术,形成了基于法向过载和滚转角速率的方向舵通道协调耦合控制方案,并通过某样例模型进行对比仿真。仿真结果表明:该方案能有效抑制侧向机动过程的侧滑角,满足机动飞行过程冲压发动机进气对侧滑角的约束需求。

In order to improve the coordination of tactical missile＇s turn process, and satisfy restriction of new type tactical missile ramjet intake on sideslip angle, the coordination control technology based on the movement coupled was studied. Combined with the classical overload control plan, this paper mainly studied the sideslip angle restriction control technology based on the three channels movement coupling, create rudder channel coordinate coupling control plan based on normal overload and roll angle speed, and carryout comparing simulation by certain type model. The simulation results show that the plan can effectively restrict sideslip angle in lateral movement process and satisfy restriction of ramjet on sideslip angle.