拦截导弹脉冲推力器点火算法研究

Yongxin Yin, Zhongming Ou, Wen Shi
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引用次数: 0

摘要

为了保证拦截导弹侧推力的控制精度,提出了一种新的脉冲推力器点火算法。针对自旋拦截导弹侧向推力不足的问题,提出了一种脉冲推力器火力方向和火力量的搜索方法。并给出了改进的遗传算法。在改进的遗传算法中,改进了遗传操作,克服了简单遗传算法中的局部优化问题。采用改进的遗传算法对脉冲推进器的火力进行优化,并对火力指令的跟踪误差进行补偿,以保证侧向推力的控制精度。仿真结果表明,该算法能有效地完成拦截导弹侧推力控制任务,并具有较好的性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Research on fire algorithm of pulse thrusters for interceptor missile
In order to ensure the control precision of lateral thrust for interceptor missile, a new fire algorithm of pulse thrusters is presented. With a view to defect of lateral thrust from spinning interceptor missile, a method to search fire direction and fire quantity of pulse thrusters is presented. And improved genetic algorithm is given. In this improved genetic algorithm, the genetic operation is amended to overcome the local optimization in simple genetic algorithm. According to an improved genetic algorithm, the fire quantity of pulse thrusters is optimized, and the track error of fire command is compensated to ensure the control precision of lateral thrust. Simulation results show that this fire algorithm can implement efficiently control mission of lateral thrust for interceptor missile as well as preferable performance.
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