摘要
针对电磁轨道发射系统打击目标时的快速反应要求,提出了一种平稳加速条件下电磁轨道发射系统射前电源时序快速计算方法。首先,根据电磁轨道发射系统的高电压、大电流、强载荷的工作特点,分析了系统平稳加速条件,提出了一种平稳加速的实现方法;然后,建立了电磁轨道发射系统平稳加速下的抛体出口速度与电源模块放电时序间模型,包括关系数据表构造、响应面模型建立及检验,在此基础上给出了射前电源时序的确定方法;最后,将该方法用于某电磁轨道发射系统电源时序的求解中。结果表明,该方法大大减少了计算时间,而且能够保证发射过程保持平稳,展示了该方法的有效性。
Aiming at the fast response of attacking target for the electromagnetic rail launcher system( EMRLS) ,a quick solu-tion method of discharge sequence of pulsed power before launch with steady acceleration was proposed.First,considering the system characteristics of high voltage,large current and heavy load,the conditions of steady acceleration were analyzed and its realization method was proposed.Secondly,a model for expressing the exit velocity of the projectile with discharge sequence of the pulsed power modules was established under the conditions of steady acceleration for the EMRLS,which includes relational data tables and re-sponse surface model.On the basis of constructing the model,an acquisition method of discharge sequence of pulsed power before launch was given.Finally,the proposed method was applied to solving the discharge sequence of pulsed power modules for an EM-RLS.The simulation results show that the method can reduce the computation time significantly and achieve the steady launch,which validate the availability of the method.
出处
《固体火箭技术》
EI
CAS
CSCD
北大核心
2015年第2期295-300,共6页
Journal of Solid Rocket Technology
基金
国家自然科学基金创新研究群体科学基金(61021002)
中央高校基本科研业务费专项资金(HIT.NSRIF.2014036)
重点实验室开放基金(HIT.KLOF.2013.081)
关键词
电磁轨道发射系统
电源模块
放电时序
平稳加速
electromagnetic rail launcher system
pulsed power modules
discharge sequence
steady acceleration