采用智能阻尼的飞航导弹过载控制

Overload control for winged missile using intelligent resistance

摘要:

首先分析了经典的飞航导弹过载控制系统结构,指出了其不足之处。然后给出了一种简单有效的基于规则的智能阻尼过载控制方法。同时,在控制设计过程中通过引入角加速度反馈相当于考虑了舵机的动态特性,使控制系统的动态性能得到进一步改善。最后,仿真结果验证了该方法的正确性和有效性。

Abstract:

First, classical overload control system structures for winged missile are analyzed, and their shortages are pointed out. Then, a simple effective overload control method for winged missile using intelligent resistance is presented. Simultaneously, the dynamics of the actuator are taking into account in the control system design process by introducing angular rate feedback, and thus the performance of the control system in transient response are further improved. Finally, simulation results show that the proposed method is right and effective.