战术导弹技术
戰術導彈技術
전술도탄기술
TACTICAL MISSILE TECHNOLOGY
2009年
3期
33-36,59
,共5页
遭毁伤导弹%弹道特性%六自由度运动方程组
遭燬傷導彈%彈道特性%六自由度運動方程組
조훼상도탄%탄도특성%륙자유도운동방정조
damaged missile%ballistic characteristic%six-free-degree movement equations
针对结构毁伤引起导弹偏航问题, 进行了遭毁伤导弹六自由度全弹道数字仿真分析.建立了导弹六自由度运动方程组, 在Matlab/Simulink实时仿真平台下开发了导弹全弹道数字仿真系统, 进行了遭毁伤导弹终点状态和飞行轨迹特性分析, 研究结果对新型反导技术发展具有一定参考价值.
針對結構燬傷引起導彈偏航問題, 進行瞭遭燬傷導彈六自由度全彈道數字倣真分析.建立瞭導彈六自由度運動方程組, 在Matlab/Simulink實時倣真平檯下開髮瞭導彈全彈道數字倣真繫統, 進行瞭遭燬傷導彈終點狀態和飛行軌跡特性分析, 研究結果對新型反導技術髮展具有一定參攷價值.
침대결구훼상인기도탄편항문제, 진행료조훼상도탄륙자유도전탄도수자방진분석.건립료도탄륙자유도운동방정조, 재Matlab/Simulink실시방진평태하개발료도탄전탄도수자방진계통, 진행료조훼상도탄종점상태화비행궤적특성분석, 연구결과대신형반도기술발전구유일정삼고개치.
Aiming at the problem of construct damage resulting in the yaw of missile, six-free-degree ballistic simulation of damaged missile is carried out. Six-free-degree movement equations for the missile are established, and ballistic simulation system for the missile is developed by real-time simulation platform of Matlab/Simulink. Based on the simulation results, terminal state and flight track of damaged missile are analyzed. This is significant to new anti-missile technology development.
