导弹与航天运载技术
導彈與航天運載技術
도탄여항천운재기술
MISSILES AND SPACE VEHICLES
2009年
6期
51-54
,共4页
倾斜发射%发射车%发射动力学%刚柔耦合
傾斜髮射%髮射車%髮射動力學%剛柔耦閤
경사발사%발사차%발사동역학%강유우합
Oblique launching%Missile launcher%Dynamic analysis of launching%Rigid-flexible coupling
基于模态综合法方法,利用ADAMS和ANSYS建立了导弹发射系统的刚柔耦合模型,通过对发射过程动力学仿真分析,获得了导弹的发射姿态和发射系统的动力学特性,分析结果通过试验进行了验证.
基于模態綜閤法方法,利用ADAMS和ANSYS建立瞭導彈髮射繫統的剛柔耦閤模型,通過對髮射過程動力學倣真分析,穫得瞭導彈的髮射姿態和髮射繫統的動力學特性,分析結果通過試驗進行瞭驗證.
기우모태종합법방법,이용ADAMS화ANSYS건립료도탄발사계통적강유우합모형,통과대발사과정동역학방진분석,획득료도탄적발사자태화발사계통적동역학특성,분석결과통과시험진행료험증.
Based on the method of component model synthesis,a rigid-flexible coupling model of missile launcher is built by the ADAMS and ANSYS.The dynamic characteristics of missile attitude and launching system have been obtained through the dynamic analysis of the launching process.Its results have been proved by tests.
