摘要
针对中远程空空导弹究竟需要多大的设计过载这一问题, 建立仿真所需的数学模型, 以空空导弹为例, 通过典型弹道和全面弹道仿真, 建立导弹需用过载随目标机动、攻击距离和离轴角变化的关系, 得出相应结论。根据仿真结果, 限定发射条件, 确定导弹需用过载最大值, 为导弹的可用过载等总体指标的设计提供依据。
In order to figure out the maximum required overload for a kind of long-range airborne missile, The corresponding mathematics modules were built up. By simulating the typical and overall ballistic trajectories, the curve of required overload changing with abaxial angle, target maneuver, and target distance was made, draw some conclusions. The given maximum required overload can be considered as the input condition for overall designs of long-range missile, such as, the available acceleration, the coefficient of promote force in blowy data, and launch condition, etc.
出处
《航空兵器》
2005年第1期8-11,共4页
Aero Weaponry
