防空导弹反弹道导弹跟踪制导规律研究和弹道仿真

利用基准优化弹道参数和滑模控制思想,构造滑动面,提出了一种新的弹道跟踪制导规律。给出了详细的推导过程,并且对所构造李雅普诺夫函数进行了稳定性证明,还进行了弹道跟踪制导数字仿真,提供了仿真弹道数据和有关弹道参数曲线。结果表明,提出的弹道跟踪制导规律是有效的,可用的。

Trajectory tracking guidance law and trajectory simulation of antiballistic missile

Parameter of optimized trajectory and variable structure with sliding modes control theorem are used to construct sliding surface, obtain a new tracking trajectory guidance law. The obtaining process is given with stability proving applied Lyapunov Function. Computer simulation for the movement of interceptor offers the trajectory data and the figure. It's shown that the tracking guidance law is reasonable and feasible.