ballistic trajectory的例句大全

The simulation of ballistic trajectory provides the foundation for gunning simulation in antiaircraft artillery.

高炮弹道仿真是高炮射击过程仿真的基础.

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A method for dim ballistic trajectory detection based on multiscale morphological reconstruction is presented.

本文提出了一种多尺度形态重构的微弱弹道轨迹检测方法.

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The paper also studied the method in measuring the burst point and tracking ballistic trajectory.

研究了PSD器件 在炸点测量和弹道跟踪方面的应用途径.

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The tracking law of ballistic trajectory is leaded by infrared camera of the early-warning satellite.

推导了预警卫星红外相机对弹道导弹的跟踪规律.

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When using the ballistic trajectory integral method to obtain the ballistic coordinate, the preci-sion of initiative shoot condition is vital.

在使用弹道积分方法求取弹丸飞行弹道坐标时，起始发射条件的准确性至关重要。

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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。

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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.

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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.

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This paper mainly experiment research and numerical analyzed the submunition ballistic trajectory condition of hard munition.

本文主要对攻坚弹药子弹弹道环境进行了初步的试验研究和数值分析.

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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；

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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。

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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。

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