Dynamic simulation of stage separation of missile based on ADAMS

Jing Nan Wang*, Li Liu

*此作品的通讯作者

科研成果: 期刊稿件文章同行评审

6 引用 (Scopus)

摘要

Using ADAMS software, dynamic simulation was done to the two-stage missile with sleeve joint. The aerodynamic forces on the missile in the course of separation were described accurately in ADAMS software. The forces between two stages were calculated. The separation was proved to be rapid and successful. The results were compared with the data which was got through the ballistic simulation, and the two results are similar. So the dynamic simulation means using ADAMS software is correct.

源语言英语
页(从-至)3512-3514+3519
期刊Xitong Fangzhen Xuebao / Journal of System Simulation
18
12
出版状态已出版 - 12月 2006

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