论文部分内容阅读
研究了空间攻击的修正比例导引规律。与根据最优控制理论获得的导引规律相比，实施比较方便。对某型反坦克导弹进行仿真结果表明，具有较高的制导精度。本方法可用于导弹总体方案设计阶段参数的选择和分析
The modified proportional navigation rule of space attack is studied. Compared with the guidance law obtained according to the optimal control theory, the implementation is more convenient. The simulation result of a certain type of anti-tank missile shows that it has high guidance accuracy. The method can be used in the design and analysis of the parameters of the missile’s overall scheme design stage