作　　者： (毕开波）; (张翼飞）; (隋先辉）;

机构地区： 大连舰艇学院导弹系,辽宁大连,116018

出　　处： 《海军航空工程学院学报》

摘　　要： 在跃升机动、蛇行机动、摆式机动和螺旋机动4种机动的变轨通用控制指令形式基础上,以拦截弹脱靶量的大小作为评判靶弹突防效果的指标,建立了末端机动靶弹突防效果的脱靶量分析模型,并提出了上述4种形式变轨突防最优参数的设计方法.在这些最优参数的作用下,导弹靶弹的机动变轨可实现最佳的突防效果,从而提升防空导弹的实战训练效果. To solve the design problem of variable trajectory maneuver of target missiles, an integrated design model was presented. By closely cooperating between the control signals of displacements and overloads, the integrated design model could make target missiles to realize the maneuver of jump trajectory, the maneuver of snake-wriggling trajectory, the ma-neuver of pendulum trajectory, the maneuver of spiral trajectory, and so on. On this basis, the penetration effect models of variable trajectory maneuvers of target missiles were studied. The design methods of the best penetration maneuvers param-eter were put forward. According to these parameters, target missiles could realize the best penetration effect, promote train effect of air defense missile.

分 类 号： [TJ760]