摘要
为了解决整流罩分离的可靠性问题,通过对采用分离弹簧的导弹整流罩安全分离的影响因素的分析,利用Admas软件对解锁不同步、弹簧刚度偏差、弹簧失效三类影响因素下的整流罩分离过程进行了动力学仿真,并对仿真结果进行了分析,得出的结论为改善导弹整流罩分离的动力学性能提供了参考。
In view of reliability of fairing separation, through the analysis of the separation spring for missile fairing, separation process car-ried out under the three categories of influencing factors that unlock is not synchronized, the bias of spring stiffness, spring failure fairing, the dynamics simulation was done by Admas, and simulation resuhs were analyzed, the conclusions provide a reference to improve the dy-namic performance of missile fairing separation.
出处
《弹箭与制导学报》
CSCD
北大核心
2013年第2期137-140,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
