摘要
应用 ADAMS动力学仿真分析软件 ,建立多管火箭发射车完全参数化的仿真模型。对发射车的多种发射工况 :不同发射角度、不同发射顺序、不同发射间隔等进行实时仿真分析 ,获取火箭弹出筒时的姿态参数 ,以及发射车各运动构件的运动特性和约束反力等。
A fully parametrized simulation model of multitube launcher is built by use of ADAMS dynamic simulation analytical software. By real time simulation analysis of various launching operational modes, such as different launching angles, different launching sequences and different launching intervals, the attitude parameter′s at exit of launch tube and the kinematic characteristics and constraining counter force of the moving parts of launcher can be gained.
出处
《导弹与航天运载技术》
北大核心
2003年第2期16-24,共9页
Missiles and Space Vehicles
