摘要
建立了火箭弹起始扰动发射动力学模型，进行了数值仿真，分析了火箭发射过程中火箭弹缺陷、发射装置振动。
The dynamics model of initial disturbance of rockets is established and the numerical simulations are carried out. Some influencing factors including rockets error, stiffness of launcher and the gap between rockets and tube are analyzed in detail and their influences quantified.
出处
《弹道学报》
CSCD
1996年第3期69-74,共6页
Journal of Ballistics
关键词
起始扰动
动力学模型
数值仿真
火箭弹
rockets, initial disturbance, dynamics model, numerical simulation
