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出 处:《弹箭与制导学报》2006年第S9期881-884,共4页Journal of Projectiles,Rockets,Missiles and Guidance
摘 要:针对某小型导弹的杀伤区高近界、低近界和低界,分析了影响因素,建立了仿真模型并进行了仿真计算,给出了各边界的空间形状与两个正交平面的杀伤区形状。最后对导弹对不同飞行距离和高度的目标拦截能力进行了分析,分析结果表明,该型导弹对超低空和临空目标的拦截能力并不理想,应适当改进导弹气动布局,增加可用过载,提高导弹对超低空和临空目标的拦截能力。Aiming at the high-near bound,low-near bound and low bound of killing scope of a small missile,factors which affect them are analyzed,the simulation model are constructed and calculated,and the space shapes of each bound and the killing scope shape of two orthogonal planes are presented.By analyzing the intercepting ability of the missile for different'flight distanee and altitude targets,the he results demonstrate that the missile doesn't have ideal intercep- ting ability for super-low-altitude and upper-approaching targets,therefore,the available overload should be increased by improving the pneumatic topology,which will improve the intercepting capacity of the missile for super-low-altitude and upper-approaching targets.
关 键 词:杀伤区高近界 杀伤区低近界 网格搜索法 超低空 临空
分 类 号:TJ762.13[兵器科学与技术—武器系统与运用工程]
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