助手标题  
全文文献 工具书 数字 学术定义 翻译助手 学术趋势 更多
查询帮助
意见反馈
   trajectory 在 武器工业与军事技术 分类中 的翻译结果: 查询用时:0.193秒
图标索引 在分类学科中查询
所有学科
武器工业与军事技术
自动化技术
航空航天科学与工程
石油天然气工业
数学
力学
计算机软件及计算机应用
气象学
电力工业
更多类别查询

图标索引 历史查询
 

trajectory
相关语句
  弹道
    Theory and Application Study on Underwater Trajectory Dynamic System Modeling of Submarine Launched Missile Carrier
    潜射导弹运载器水弹道动力系统建模及其应用研究
短句来源
    ALGORITHM FOR OPTIMIZING AIR-TO-SHIP MISSILE TRAJECTORY
    空舰导弹弹道优化算法
短句来源
    APPLICATION OF THE QUATERNION METHOD IN FLIGHT TRAJECTORY SIMULATION OF TACTICAL MISSILES
    四元数法在战术导弹飞行弹道仿真中的应用
短句来源
    SCHEME TRAJECTORY RESEARCH OF LONG-RANGE ANTITANK MISSILE
    远程反坦克导弹方案弹道研究
短句来源
    One Method for Determining Analytic Expression of Trajectory Data
    确定弹道诸元解析表达式的一种方法
短句来源
更多       
  轨道
    THE INTERIOR BALLISTIC PARTICLE TRAJECTORY MODEL AND ITS NUMERICAL CALCULATION
    内弹道颗粒轨道模型及数值计算
短句来源
    AN AXISYMMETRICAL PARTICLE TRAJECTORY MODEL AND ITS SIMULATION
    轴对称两维颗粒轨道模型
短句来源
    Gradient projection descent algorithms for real-time computation of trajectory optimization:real-time computation methods for optimization of air defence missile trajectory
    轨道优化实时计算的梯度投影下降算法——防空导弹轨道优化的实时计算方法之二
短句来源
    The mathematical model of the intercept problem is derived from the spacial ballistic trajectory computational model and the orbit prediction model.
    在建立了六自由度空间弹道计算模型和轨道预测模型后,对拦截问题进行数学建模,并分析了牛顿迭代法求解拦截问题的可行性。
短句来源
    Summary of the vehicle trajectory optimazation and guidance law
    飞行器的轨道优化与制导规律研究综述
短句来源
更多       
  “trajectory”译为未确定词的双语例句
    Dynamic Correction for the Ideal Trajectory of the Proportional Guidance Missiles
    比例导引导弹理想弹道的动态修正
短句来源
    A Method for Trajectory Identification and Fusion in Multitype Radars
    多种类雷达航迹辨识及融合的实用方法
短句来源
    Generation of TBM′s Trajectory in the Simulation of Anti-TBM Battle
    反TBM作战仿真中TBM弹道的生成
短句来源
    Study on the Bayesian Method of Trajectory Unanimity Test
    成组交替对比射击的Bayes评定方法研究
短句来源
    Calculation Status Design of Statistic Trajectory for Hitting Target with Uniform Design Method
    用均匀设计法设计统计打靶的计算情况
短句来源
更多       
查询“trajectory”译词为用户自定义的双语例句

    我想查看译文中含有:的双语例句
例句
为了更好的帮助您理解掌握查询词或其译词在地道英语中的实际用法,我们为您准备了出自英文原文的大量英语例句,供您参考。
  trajectory
The key to coordination is gait trajectory tracking control.
      
P-type open-closed-loop iterative learning control (ILC) is not based on model parameters and has advantages in both open-loop and closed-loop ILC; so this paper proposes a complex robot gait trajectory tracking.
      
The simulation results indicate that the dynamical sliding-mode controller can not only track the given trajectory correctly but also reduce the chattering of sliding-mode control system considerably.
      
To precisely implement the force control of robot manipulators in an unknown environment, a control strategy based on fuzzy prediction of the reference trajectory in the impedance model is developed.
      
The elliptical trajectory of the driving tip is formed by exciting the longitudinal and bending vibration with phase difference, which generates thrust force and normal force, respectively.
      
更多          


Hollow projectile is virtually a thin-walled tube, also known as tube projectile. It is characterized by its light weight, high muzzle velocity and desired aerodynamic behaviour. Hence it provides the advantages of lower impulse, straighter trajectory, smaller dispersion and excellent penetrating power.

空心弹丸基本上是一个中空薄壁圆管(因而又称管式弹丸),它的重量轻、初速高、气动性能好,从而使得膛口冲量小、弹道低伸、散布小,并且具有优越的侵彻效果。本文在前人研究成果的基础上,结合我们的试验研究情况,比较详细地叙述了这一新弹种的低阻性能、散布精度和侵彻性能;从理论上分析对比了空心弹丸和实心弹丸的陀螺稳定性;给出了空心弹丸的阻力特性近似估算方法;最后,就这一新弹种在弹药上应用的可能性问题提出了一些看法和建议。

This paper presents a method for employing electronic computer of small and medium size to compute and select the angular velocity ω_(t0) of self-destruction device, and to determine the principal structural parameters of the device. In this method, firstly we compute the exterior trajectory and the rotational angular velocities of the projectiles along the trajectory, and then we obtain the curve ω-t of angular velocities vs. time of flight. Through the analysis of ω-t curve family under various...

This paper presents a method for employing electronic computer of small and medium size to compute and select the angular velocity ω_(t0) of self-destruction device, and to determine the principal structural parameters of the device. In this method, firstly we compute the exterior trajectory and the rotational angular velocities of the projectiles along the trajectory, and then we obtain the curve ω-t of angular velocities vs. time of flight. Through the analysis of ω-t curve family under various angles of fire, we select a ω_(t0)~* which can meet the tactical requirements. For various numbers and diameters of the steel balls, we can compute the curve of angular velocity ω_(t0) of self-destruction vs. oblique angle α of the bevel shaped edge of sleeve (Fig. 2) and we get a group of curves. Based on the ω_(t0)~* selected from the tactical requirememts, we can determine suitable structural parameters i, d and α. With this method we can easily reveal the conditions of the dispersion of the burst points and the relationship between the positions of burst points of self-destruction and the minimum angle of fire θ_(0min) under various angles of fire θ_0 so as to solve the problem of optimum design which needs large amount of calculations and requires a few but very comprehensive influencing factors.

本文提出了一种利用中小型电子计算机论证选择离心自炸机构自炸角速度ω_(t0)~*。及设计确定钢珠离心自炸机构基本结构参量的方法。这种方法是首先计算外弹道和弹丸沿弹道的旋转角速度ω,然后输出旋转角速度对于时间的曲线ω-t,通过对不同射角下ω-t曲线族的分析,选择战术要求的ω_(t0)~*。对不同的钢珠数目i,不同的钢珠直径d,可以计算出自炸角速度ω_(t0)与倾角α(参见图2)的关系曲线,输出这个曲线族,根据战术要求选定的ω_(t0)~*。即可分析确定合适的结构参量i,d及α。这种方法便于看清各种不同射角θ_0时自炸炸点分布的情况及自炸炸点位置与最小射角θ_(0min)的关系。从而可以解决这种计算量大、要求考虑全面而因素又不太多的优化设计问题。

This paper is continuous part of previously published paper[1]. Some aspects about guidance for genuine MIRV is mainly discussed. They are the guiding scheme for space maneuvering vehicle, the roll control program of attitude for the body, the design of maneuvering penetrating trajectory in longitudinal plane and the mechanization of perturbed guidance equation.

本文是前已发表的文章[1]的续篇。主要讨论有关全导式分导制导的若干问题。它们是。空间机动飞行器的导引法,弹体的滚动姿态控制方案,纵平面内机动突防弹道的设计以及摄动制导方程的编排。

 
<< 更多相关文摘    
图标索引 相关查询

 


 
CNKI小工具
在英文学术搜索中查有关trajectory的内容
在知识搜索中查有关trajectory的内容
在数字搜索中查有关trajectory的内容
在概念知识元中查有关trajectory的内容
在学术趋势中查有关trajectory的内容
 
 

CNKI主页设CNKI翻译助手为主页 | 收藏CNKI翻译助手 | 广告服务 | 英文学术搜索
版权图标  2008 CNKI-中国知网
京ICP证040431号 互联网出版许可证 新出网证(京)字008号
北京市公安局海淀分局 备案号:110 1081725
版权图标 2008中国知网(cnki) 中国学术期刊(光盘版)电子杂志社