最大射程

导弹最大射程Bayes估计的分析和改进

Analysis and improvement of some Bayes estimate for the maximum range of a missile

用Matlab从阻力系数和物体质量对斜抛运动的轨迹和最大射程抛射角影响方面进行数值研究和分析。

Applying matlab , in this paper the number research and analysis have been made in the aspect that the air resistance coefficient and the object mass affect the projectile motion .

本文讨论最大射程的统计评定方法。

This paper discusses the statistical detection methods for the maximum range .

最大射程与最佳抛射角关系新探&发散思维在解决抛体运动问题中的运用

Apply Divergent Thinking on Solving Problem of Projectile Motion

榴弹炮最大射程50公里（采用火箭助推炮弹）。

Max range of the howitzer is50 kilometers ( with rocket assisted shells ) .

一种固体导弹最大射程评定方法

Maximum Range Evaluation Method for Solid Missiles

一些评定液体弹道式导弹最大射程的新的统计方法

Some new statistical methods for evaluation of the maximum range of a liquid ballistic missile

从高于它最大射程的大炮上射击。

Fire from a cannon fired at an elevation greater than that for the maximum range .

基于前者的计算结果分析了初始条件对最大射程弹道的影响。

The numerical results of first kind trajectories show the influence of initial condition on the maximum range trajectories .

模拟给出四个不同能量的电子束在聚苯乙烯材料中的最大射程，并与实测外推得到的最大射程进行比较。

Simulate practical range of electron beamss in polystyrene material under four different energy conditons , and compare it with practical extrapolated electron range .

在大口径远程榴弹设计中，在保证弹丸具有足够的威力，飞行稳定性和发射强度的前提下，使弹丸具有最大射程是一个很有意义的问题。

Designing large calibre and long range projectiles , with maximum range , ample power , flying stability , and launching strength , is a significant problem .

空中点火机构动态延期时间研究是底排&火箭复合增程弹实现其最佳增程弹道，提高最大射程密集度的重要环节。

Research on the dynamic delay-time of Hybrid igniting-device in the air is the basis of implementing it 's the best trajectory and improving its max cannon-shot denseness .

首先利用同伦方法的大范围收敛特性，构造原最大射程问题的同伦映射，推导了最大升阻比控制规律，以最大升阻比弹道作为初始解轨迹。

The homotopy map for maximum range problem is built by using homotopy method with a large scope convergence property , and the control law of maximum lift-drag ratio is deduced .

针对弹道式导弹整个飞行弹道的多种约束要求，建立了弹道最大射程优化的数学模型，在MATLAB/SIMULINK环境中，建立相应的仿真模型。

Considering constrains of the whole flight trajectory of the ballistic missile , a mathematical model of maximum range optimization was built , a corresponding simulation model was also built under the MATLAB / SIMULINK environment .

为了解决铅球适宜投出角度公式与实践偏离的问题，分析了铅球成绩与抛体最大射程的函数关系，得出了最大成绩定理、新最佳投出角度公式和最佳出手角度标志线参数式。

In order to solve the problem of deviation of suitable angle and the practice of shot put , the author analyzes the function relation between performance and the maximum projectile range , draws the best result theorem that is new optimum angle formula and sign line parameter .

首先分析了影响一维弹道修正引信阻尼弹道系数选取的主要因素，提出了弹道解算时间和最大射程修正量的确定是计算最佳阻尼弹道系数的的前提。

This paper analyzes the dominating factors that influence damping ballistic coefficient of one dimension trajectory correction fuze , brings forward that it is a precondition of optimize and simulation for damping ballistic coefficient to work out the time of calculating ballistic trajectory and the distance of maximum range correction .

弹道拟合技术在反舰导弹最大有效射程评估中的应用

The Application of Ballistics-fit Method to the Evaluation of Maximum Flight Distance of Anti-ship Missile

因此，当发射角为45°时，有最大水平射程。

Thus the maximum horizontal range is attained when the departure angle is 45 ° .

最大有效射程双35毫米武器的约4000米，与循环率火警550策略/分钟。

The maximum effective range of the twin 35 mm weapons is about 4,000 m , with a cyclic rate of fire of 550 rds / min.

发射装置是前面进弹而且能发射35毫米高爆（HE）和高爆反坦克弹药（HEAT）具有最大400毫米射程。

The launcher is front-fed and can fire35mm high-explosive ( HE ) and high-explosive anti-tank ( HEAT ) rounds with a maximum range of400m .

为最大限度发挥直升机载激光半主动制导的潜能，对本机发射导弹本机照射在最大射程和近距离射击存在问题进行了研究。

We 've discussed laser systems which operate in the maximum and near range with host helicopter launching missile and laser designator , in order to develop local helicopter Laser semi-active guidance potential power .