摘要
针对中远距空空导弹发射后不管的控制需求,对中远距空空导弹拦截目标的弹道进行了优化设计;在进行弹道规划时将导弹的飞行过程分为中制导段、中末制导交接段和末制导段,分析了不同飞行阶段的制导控制要求,在此基础上完成了各个阶段弹道规划,并给出了实现途径。
The optimum design of trajectory is given for middle-long-range air-to-air missile in this paper.In order to design the trajectory,the whole flight period of missile is divided into three stages: midcourse stage,takeover stage and terminal stage.Then the control requirement of each flight phase is analyzed.On the basis of this analysis,the trajectory planning is proposed and trajectory realization method is given.
出处
《四川兵工学报》
CAS
2013年第5期38-39,43,共3页
Journal of Sichuan Ordnance