基于虚拟样机的多管火箭起始扰动仿真系统

Simulation Analysis System for MLRS Initial Disturbance Based on Virtual Prototype

依据多管火箭起始扰动计算原理,对比分析了采用虚拟样机技术进行多管火箭起始扰动仿真分析方法相对于传统测试方法的优越性;结合对ADAMS软件的二次开发,介绍了多管火箭起始扰动仿真分析系统的功能及软件实现;通过实际算例,验证了系统的正确性和有效性。

Based on the analysis of initial disturbance principle of multiple launch rocket system, the advantages of virtual prototyping over traditional test method were proposed. Combining with redevelopment of ADAMS, the function and implement of the dynamics analysis on MLRS initial disturbance simulation system was introduced. A benchmark was given to validate the correctness of the model and convenience of the system.