某型滑翔增程靶弹方案弹道设计OA北大核心CSTPCD
Design of Project Trajectory for Glide Range-Extended Target Missile
针对某滑翔增程靶弹的无动力特性,综合各方面因素,提出一种具有近似平飞段的方案弹道.选择相关参数,设计了一种具有近似平飞段的高度变化律,提出了改进的攻角表达式,得到无动力靶弹三自由度铅垂平面的运动模型.数字仿真证明,这种方法合理可行,满足了靶弹各项战技指标,实现靶弹的近似平飞,方案弹道能较好地追踪给定高度变化,具有较高的工程应用价值.
According to the power-free characteristics of glide range-extended target missile, one project trajectory scheme approximate level flight section is proposed based on the comprehensive factors of various aspects. Relative parameters are selected for designing a height change law approximate to level flight section, proposing the formula of attack angle, and obtaining the motion model of the three degree of freedom vertical plane of power-free target missile…查看全部>>
王洪强;邵晓巍;杨黔龙;沈学霖;段登平;周刚
上海交通大学,上海200240西北核技术研究所,陕西西安710024上海交通大学,上海200240西北核技术研究所,陕西西安710024西北核技术研究所,陕西西安710024上海交通大学,上海200240
军事科技
靶弹近似平飞方案弹道
target missileapproximate level flightprodraft trajectory
《现代防御技术》 2012 (2)
27-31,5
总装备部重点项目(21010901)
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