ballistic trajectory的例句大全

Study on Ballistic Trajectory Simulation in Antiaircraft Artillery

高炮弹道仿真的研究

The estimation for maneuvering tactical ballistic missiles ( TBM) trajectory in its terminal phase is an important part of the modeling of modern air-defense C~ 3I system. It has direct effects on the intercept precision and probability of anti-TBM operation.

TBM末端机动弹道的预测是现代防空C3I系统建模中重要的组成部分，它直接影响着反导武器系统对TBM拦截的精度与概率。

Through systematical analysis, a mathematical model has been established for early warning satellite to forewarn the TBM ( Tactical Ballistic Missile) trajectory.

建立了预警卫星系统对战术弹道导弹（TBM）弹道进行预警的一种数学模型，其中包括预警卫星系统信息库的信息模型；用预警卫星探测信息确定TBM坐标的模型；

Based on the analysis of flight trajectory of ground-to-ground ballistic missile, a simplified mathematical model for missile impact point calculation was set up.

在分析地地弹道导弹射击弹道的基础上，建立了其落点计算的简化数学模型。

Research on Algorithm of Ballistic Parameter for Trajectory Correction Fuze and Analysis of the Precision of MIMU

基于MIMU的弹道修正引信弹道参数解算及对MIMU的精度要求

After-working impulse is main source to ballistic missile flight trajectory error and hit error.

后效冲量误差是引起弹道导弹飞行弹道误差和命中误差的一个重要误差源.

The ballistic parameters are measured during the earlier stage of the booster phase. The impact deviation can be predicted based on the difference between measurements and reference trajectory. Thus the azimuth angle and action times of impulse mortars are to be determined.

通过测量主动段前期的弹道参量，比较同一时刻其与基准弹道的偏差量，再估算得到落点偏差，确定脉冲作用方位角和作用次数。

Trajectory estimation by geostationary early warning satellite is important in ballistic missile defense. Staring trajectory estimation algorithm is discussed with the help of nonlinear KALMAN filter based on Stirling interpolate approximation.

地球静止轨道预警卫星弹道重构是弹道导弹防御的一个重要环节，利用基于Stirling插值逼近的非线性KALMAN滤波方法，对凝视型弹道重构算法进行了研究。

Solving ballistic missile trajectory design elevation Angle is presented, the procedure of the method of engineering program design elevation Angle.

弹道导弹的弹道求解就是设计俯仰角程序，文中给出了俯仰角程序设计的工程方法。

A kind of new interior ballistic model ── particle trajectory model is introduced in this paper.

该文介绍了一种新型的内弹道两相流模型&颗粒轨道模型。

Considering of SRM internal ballistic property and rocket trajectory, in this paper the influence of the parameter of SRM grain configuration, chamber and nozzle design on the motor property and overall rocket performance of the parameter is analyzed.

在综合考虑固体火箭发动机内弹道性能和火箭外弹道性能的情况下，融内外弹道仿真分析为一体，系统分析了发动机装药、燃烧室和喷管设计参数对发动机性能及全弹性能的影响。

Research on Simulation Model of the Antiballistic Missile System By use of direct trajectory optimization method, the selection of overall design parameters of an anti ballistic missile for a 1?

应用求解非线性规划问题的直接方法，针对一种典型的目标弹道（1000km），对一种方案反战术弹道导弹进行了总体参数优化设计研究.研究中考虑了：发动机特性参数的变化；

Ballistic Model and Simulation of a Portable Antitank Missile Steering to Hit on Top of the Tank at Terminal Trajectory

击顶折转轻型反坦克导弹弹道建模及仿真

The GPS technique used for the high accuracy measurement of the outside ballistic track provides an unprecedented technique support in outside trajectory designing, checking and revising for the trajectory fights battle weapon and precision attack military tactics weapon, and improving the weapon fights accuracy.

GPS技术用于外弹道轨迹的高精度测定，为弹道打击战役武器及精确打击战术武器的外弹道设计、校验及修正，为武器打击精度的提高，提供了前所未有的技术支持。

To simplify the computation, the estimate equations of trajectory parameter of boost phase, crossover phase and maneuvering phase in ballistic missile's flying were brought out by approximate treatment according to the motion equation of mass center for missile in this paper.

为简化计算，根据导弹的质心运动方程，通过近似处理导出了导弹机动飞行中助推段、跨越段和机动段弹道参数的估算公式。

Then, use two methods to make the simulation. The result shows that the trajectory prediction method based on parameter identification with high generality, rapidity and accuracy can provide a basis for ballistic deflection correction and trajectory control.

结果表明，基于参数辨识的弹道预报具有通用性、快速性和准确性，可以为弹道修正及弹道控制提供基础。

A kind of new ballistic model ── particle trajectory model is introduced in this paper.

该文介绍了一种新型的内弹道两相流模型─颗粒轨道模型.

A rapid iteration algorithm adapting to ballistic missile trajectory design is presented.

摘要提供了弹道导弹弹道设计的一种快速迭代方法和模型.