The Study of Interference between Bomb and Plane and Seperating Ballistic Arm Deflection by Airborne Radar and Its Detection as Separation from Carrier

  • 航空弹药机弹干扰和分离弹道研究机载雷达对反辐射导弹诱偏及弹机分离时的检测识别
  • 来源:互联网摘选更新时间:2026-07-14 20:39:28

  • 重点词汇
  • carriern.运输工具;搬运人;军车;运输舰;航空母舰;运输公司;携带病菌者;载物架;通信公司;互联网公司;
  • armn.臂;手臂;扶手;上肢;袖子;分部;臂状物;狭长港湾;战事;权力;
  • separationn.分离,分开;间隔,距离;[矿]分选;(夫妇)分居;
  • theart.这个;指已提到或易领会到的人或事物;指独一无二的、正常的或不言而喻的人或事物;用以泛指;与形容词连用,指事物或统称的人;用于姓氏的复数形式前,指家庭或夫妇;(指特定用途的事物)足够,恰好;每,一;当前的,本,此;(重读,表示所指的为知名或重要的人或事物)
  • radarn.雷达;雷达装置;无线电探测器;
  • betweenprep.在…之间;介于…之间;往返于;共享;一起;
  • airborneadj.空运的,飞机载的;航空的;空气所带的;空气传播的;
  • deflectionn.偏斜,偏移,歪曲;偏斜度,偏角;
  • 相关例句
1、

For oblique penetration problem at a large incident angle, a new understanding is obtained that the projectile may occur reverse deflection, and after the deep analysis it is found that ballistic deflection is caused by different degree of damage of the target around the projectile.

对大倾角斜侵彻问题有了新的认识,弹体在侵彻过程中可能发生反向偏转,深入分析后得到,弹道偏转是由于弹体周围靶板的损伤程度不同引起。

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3、

This azimuth motion is known as the ballistic deflection error. Study on rotor load of vertical shaft impact crusher based on ADAMS

这种绕方位轴的运动称为冲击偏差。基于ADAMS的立轴冲击式破碎机转子载荷

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4、

Stress, frame mode, liquid dame, circuit and error, etc, which are closely related to gyroscope, are analysed in detail, so the designed gyroscope can meet the practice demand in ballistic correction.

详细地分析了与陀螺性能密切相关的应力、结构模态、流体阻尼、电子电路、误差等,使所设计的陀螺满足弹道修正的实际需要。

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5、

Such tasks have been finished as follows: 1. Understanding the correction process, the rigid body's ballistic correction model is established.

了解炮弹的修正过程,建立了基于刚体运动的弹道修正数学模型。

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6、

CZ-2E Ballistic Correction for High Altitude Wind

CZ-2E火箭高空风弹道修正

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7、

The roles that electro-optical technology plays in target acquisition and fire control and ballistic correction are pointed out.

指出光电技术在目标获取、发射控制、弹道修正等方面所起的作用。

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8、

The model can be applied further to ballistic correction, parameter optimization and ballistic simulation of TSP systems.

该模型可进一步用于末敏弹系统的弹道修正、参数优化和弹道模拟。

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9、

Firing Data Calculation and Ballistic Correction of Rate Fire-control System based on Deck Coordinates

甲板坐标系下速率火控射击诸元解算及弹道修正

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10、

Based on the practice in ballistic correction, the paper carried through gyroscope's system analysis and design.

论文基天弹道修正的实际应用,对微陀螺进行了系统分析与设计,主要完成了以下几方面的工作。

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11、

Marine Launched Accurately Guided Ballistic Missile Will Lead to Far-reaching Transform of Future Sea Battle

海射精确制导弹道导弹引发未来海战的深刻变革

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12、

The dynamic balance speeds of the rocket stored for 5 years in south and north area are measured by ballistic pendulum method and the dynamic impulses are calculated. The experimental results are disposed and analyzed based on rank sum test method.

实验测定了已经在南方和北方2个地区贮存5年的火箭弹动平衡速度,计算了动平衡冲量,并利用秩和检验方法对实验结果进行了处理与分析。

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13、

Transient and average thrust are two important performance parameters of pulse detonation engine. The principle and system structure of direct measurement method and indirect measurement methods ( including thrust wall pressure integral method and ballistic pendulum method) are introduced.

针对脉冲爆震发动机瞬时推力、平均推力测量问题,介绍了直接测量法和间接测量法(包括推力壁压力曲线积分法和抛物摆法)的测量原理及系统构成。

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14、

Then it analyzes the swing problem with two models, which are variable pendulum model and ballistic pendulum model that is based on the conversation law of momentum.

分别使用基于变长摆和基于角动量定理的定轴摆的两种摆动模型分析风摆问题,并列出风摆方程,给出数值解法。

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15、
16、

Using ballistic pendulum test, the transients of impact forces, displacements and energy absorbing are estimated.

利用冲击摆锤试验,测定了冲击力、冲击点位移以及能量转换的瞬态值。

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17、

Ballistic missile technology and rocket science.

弹道技火箭研究。

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18、

Flexible Multi-body Simulation of Brake System BALLISTIC MODEL OF FLEXIBLE ROCKET

制动器多柔体仿真分析柔体火箭弹道模型的建立

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19、

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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20、

At first the ballistic model of rocket projectile vertical launch is established, then it researches lift-to-drag ratio and influence of the angle of flight path on the firing range.

首先建立了火箭弹垂直发射的弹道模型,然后研究了升阻比、弹道倾角等参数的变化对火箭弹射程的影响,并分别对这两种情况进行了仿真。

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