An optimization design of small rollingmissile controller parameter based on genetic algorithms was developed.
提出了一种基于遗传算法的小型旋转弹控制器参数优化设计方法。
2
The mechanism of dynamic instability of rollingmissile was analyzed by describing the dynamics of rollingmissile as a closed loop with dynamic negative feedback.
将滚转导弹动力学系统描述为一个具有动态负反馈的闭环系统,分析了滚转导弹动态失稳的机理。
3
Considering the difference of the rollingmissile and the non-rollingmissile, the mechanism of rollingmissile control force and the control theory of rollingmissile was analyzed rigorously.