导弹靶弹弹道机动变轨通用控制指令设计  

Design of General Control Instructions for Variable Trajectory Maneuvers for Target Missiles

作　　者：毕开波[1] 张翼飞[1] 张传刚[1] 

机构地区：[1]海军大连舰艇学院,辽宁大连116018

出　　处：《导航定位与授时》2016年第4期30-37,共8页Navigation Positioning and Timing

摘　　要：导弹进行一定强度的机动飞行,就能够提高突防能力,因而,在军事训练中需要具有末端机动变轨能力的靶弹。针对靶弹机动变轨弹道的设计问题,提出变轨通用控制指令设计形式,利用此设计可使靶弹位移与过载指令控制信号协调配合,控制靶弹实现跃升机动、蛇行机动、摆式机动和螺旋机动等变轨形式。通过仿真证明,此设计的变轨弹道通用控制指令,可以满足靶弹跃升机动、蛇行机动、摆式机动和螺旋机动等各种变轨形式的弹道设计要求。To solve the design problem of variable trajectory maneuver of target missiles,an integrated design model of variable trajectory maneuver is presented. By closely cooperating between the control signals of displacements and the control signals of overloads,this integrated design model can make target missiles to realize the maneuver of jump trajectory,the maneuver of snake-wriggling trajectory,the maneuver of pendulum trajectory,the maneuver of spiral trajectory,and so on. the variation form of optimal maneuver parameters and the combination form of basic maneuver trajectories are realized. Simulation results show the effectiveness of the proposed methods.

关 键 词：导弹靶弹 机动变轨 过载控制 

分 类 号：TJ760[兵器科学与技术—武器系统与运用工程]