弹道修正防空弹药飞行最优控制方法研究

结合高炮弹药修正的特点，利用最优控制理论基于能量消耗最少的准则推导出弹道特征参数的控制策略。通过仿真得到了在固定起点和固定终点条件下，弹道修正弹最优飞行弹道倾角和速度随时间的变化曲线，以及弹丸变轨需要侧向过载的变化情况。结果表明侧向过载的变化情况符合脉冲力的变化规律，反映出该控制方法在一定程度上可满足弹道修正弹脉冲力的控制要求。

Optimal Control Solution in Antiaircraft Trajectory Correction Projectile

Based on the particularity of the antiaircraft trajectory correction projectile, a control strategy on characteristic parameters of the trajectory is derived from the guide line of least energy cost in this paper. On the condition of fixed starting point and fixed terminal point, the variation rules of optimal trajectory oblique angle, velocity and lateral overload for trajectory correction are obtained from the simulation. The simulation result shows that the variation of lateral overload matches the rule of pulse variation, which proves that the proposed solution satisfies the need of the pulse trust for trajectory correction projectile.