1) ballistic body
弹道体
2) flexible ballistics
柔体弹道
1.
Based on the coupled dynamic model for the spatial motion of 6 degrees of freedom and the dynamic deformation of the body, the flexible and dynamic equations are analyzed by the mode methods of vibration, the equations of flexible ballistics in the model form are obtained.
从弹箭空间六自由度运动和动态变形耦合的动力学模型出发 ,利用振动模态方法对弹体的柔性变形和动态变形耦合的动力学模型出发 ,利用振动模态方法对弹体的柔性变形和动力学方程组进行了分析 ,得到了柔体弹道的模态化方程组 ,以此为基础推导了弹轴摆动和弹性振动耦合的运动微分方程
3) three body trajectory
三体弹道
1.
Based on three body trajectory calculation the emission time scale of light particles has been extracted from correlation function of two particles at small relative momentum.
通过与三体弹道模型的比较 ,从关联函数提取了轻粒子的发射时间 。
4) rigid body trajectory
刚体弹道
1.
The six-free degree rigid body trajectory equations are established, based on the analysis of the forces and the moments acted on the projectile.
本文以某滑翔增程炮弹为研究对象，定义了描述其运动的相关坐标系，分析了其所受外力及力矩，建立了六自由度刚体弹道模型，编制了滑翔增程弹全弹道仿真程序。
5) solid ballistic missile
固体弹道导弹
1.
Application of collaborative optimization method to conceptual design of solid ballistic missile;
协同优化在固体弹道导弹概念设计中的初步应用
2.
In this paper,an approach to depleted shutdown closeloop guidance navigation method for solid ballistic missile is researched.
文中研究了固体弹道导弹耗尽关机闭路制导导引方法,推导建立了一种适用于无推力终止系统工作的固体弹道导弹在要求能量随机耗尽条件下的闭路制导导引模型,并进行仿真计算分析,论证了方案的正确性和可行性。
3.
in this paper, an approach to depleted shutdown guidance for solid ballistic missile is described.
本文研究了固体弹道导弹耗尽关机制导方法，提出了一种适用于无推力终止系统工作的固体弹道导弹。
6) anti-ballistic missile system
反弹道导弹体系
补充资料：半硬壳式弹体(见弹道导弹弹体)
半硬壳式弹体(见弹道导弹弹体)
semi-hard-shelled missile body
bQn yingkeshi dan桩半硬壳式弹体(semi一hard一shelled、ssilebody)见弹道导弹弹体。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条