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The angle of attack, pitch angle and velocity at shifted point for typical trajectory were calculated.

给出了两种控制方法的导引律,计算了典型弹道的攻角、俯仰角和交班点速度等参数。

With this, Chandrayaan-1 entered the Lunar Transfer Trajectory with an apogee of about 380,000 km.

与此,被输入月球调动弹道的Chandrayaan-1以远地点大约380,000公里。

With the development of computer technology, mathematical simulation is an important way in studying the interior ballistics of guns now.

随着计算机技术的发展,数学仿真已成为研究火炮内弹道的重要手段。

As a result, it shows thatthe static or dynamic subsystem optimum alone is not equal to the system optimum. Three initial value problems met in the optimal design of flying vehicle are studied andconclusions are derived that: orthogonal test method can be adopted to decide the initial valueof static optimization problem, some mathematical techniques can be used to deal with thecostate variables of Maximum Principle and decide the initial value of the costate variable,the indirect method can be used to get the analytical solution under ideal case to guide thechoice of the initial control curve in the direct method. With some numerical examples oftrajectory optimization, it shows that all these methods are useful not only in accelerating theconvergence but also in converging to the global optimum.

针对飞行器优化设计中的三种初始值问题进行了研究,以远程弹道导弹弹道的工程优化为例说明,对于静态优化问题,采用正交试验法选取初始值,不仅可以大大加快收敛的速度,而且更有可能收敛到全局最优解;以气动力辅助变轨问题为例说明,用共态变量的一阶泰勒级数展开可以解决极大值原理中共态变量初值难于确定的问题;以二级弹道导弹的主动段弹道优化为例说明,利用间接法在理想情况下得到的解析解来指导直接法初始控制曲线的选择,将大大有利于提高直接法的收敛速度。

This paper presents experimental and computer simulation studies of the throwing system structure of Airborne dispenser.

本文进行了机载布撒器抛撒系统结构设计,子弹散布规律和内外弹道的计算机仿真技术研究。

The action mechanism of the stun gun is analyzed in detail and the scheme design of the stun gun system is completed. With the SolidWorks software, three-dimensional model of the system has been constructed. The characteristics of the interior ballistics of the proposed scheme of stun gun are analyzed and the corresponding interior ballistics model is proposed. The numerical computation of the interior ballistics is also conducted. According to the functions of the electrical module ,the circuit is designed and the security and reliability of the system is analyzed. At last, the test scheme of the system is proposed and some experiments are carried out which validate the feasibility of the designed system.

论文中分析了电击枪的机理,完成了系统方案的设计;用SolidWorks软件建立了三维实体模型,分析了所提方案电击枪的内弹道的特点,建立相应的数学物理模型,并进行了内弹道分析计算;根据电子模块所要实现的功能设计了硬件电路;对设计的方案进行了安全性和可靠性的分析,最后拟定了试验的方案并进行了试验研究,验证了设计方案的可行性。

The experimental results show that the shape of the pellet has significent influence on the hydro-trajectory stability.

实验结果表明,弹丸形状对入水弹道的稳定性有重要影响。

ARZT: Do I, do I know about trajectories?

我知不知道一些关于弹道的东西?

Based on the analysis of working process of ejection gun of rocket ejection seat ,the physical and mathematical models of interior ballistics of ejection gun were established and the interior ballistics parameters of a rocket eject seat were validated by test and calculation.

在分析火箭弹射座椅弹射动力系统的工作过程的基础上,建立了其内弹道的物理模型和数学模型,并对某型火箭弹射座椅弹射动力系统内弹道进行了试验验证与计算,试验所测膛内气体压力随时间变化曲线与计算曲线基本吻合,弹射过程最大压力pm、工作时间tg、出口压力pg和出口速度vg分别为24.20(24.57)MPa,157(155)×10-3s,22.27(21.83)MPa,16.61(16.59)m.s-1,各特征参数的计算值最大误差小于3%。

As the airborne missile is controlled on two different mod es, different influence of helicopter downwash flow on its initial trajectory is researched.

研究了导弹在两种不同控制模式下,直升机下洗流场对其初始弹道的影响。

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Do you know, i need you to come back

你知道吗,我需要你回来

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