1) range correction projectile
射程弹道修正弹
1.
The mass center motion equations of a damp-increasing range correction projectile were established by the concept of damp-increasing coefficients.
用增阻系数的概念,建立了增阻式射程弹道修正弹的质心运动方程组。
2) trajectory correction projectile
弹道修正弹
1.
EMC design of trajectory correction projectiles rotation angle measurement system;
弹道修正弹滚转角测量系统电磁兼容性设计
2.
The trajectory correction projectile model using impulse was established.
建立了采用脉冲力控制的弹道修正弹飞行弹道模型。
3.
In order to improve the hit efficiency of antiaircraft projectile for maneuvering target,the two-dimensional trajectory correction projectile is studied.
根据提高高射弹丸对机动目标命中率的实际需求,研究了空射型二维弹道修正弹。
3) trajectory correction munition
弹道修正弹
1.
The composition and the principle of millimeter wave(MMW) remotely controlled trajectory correction munition(RCTCM) system are researched.
讨论了毫米波遥控指令弹道修正弹系统的组成和工作原理;分析了远程低成本精确火力打击和防空反导2种模式下,对该系统在作用距离、修正能力等方面的性能要求。
2.
The conception of carrier-based double-purpose MMW remote controlling trajectory correction munition(RCTCM) is put forward and the system structure is given.
分析了舰载火炮武器作战任务的发展方向,提出了双用途舰载毫米波遥控指令弹道修正弹系统的概念,并给出了系统结构。
4) course correction projectile
弹道修正弹
1.
The makeup of course correction projectile weapon system and its working principle were studied,the models of impulse force and impulse moment were established,the pursuit guidance laws used for course correction were analyzed and the method of establishing 6-DOF trajectory model of course correction projectile was presented.
对弹道修正弹武器系统组成和工作原理进行了研究,建立了脉冲作用力及力矩模型、分析了弹道修正使用的追踪制导律,提出了建立其六自由度弹道模型的方法,利用弹道修正弹六自由度弹道仿真程序对末段修正典型弹道、探测器光轴运动轨迹以及脉冲作用点对脱靶量的影响等进行了仿真,计算结果表明在弹体质心附近使用直接脉冲控制力对末段弹道进行修正可以达到较好效果,采用速度追踪方式能够得到较小的脱靶量。
5) trajectory correction projectiles
弹道修正弹
1.
A rotation angle identification model of trajectory correction projectiles is constructed.
建立了航用弹道修正弹滚转角辨识系统数学模型,利用向弹上引信装定的初始信息及磁阻传感器探测到的地磁信息,使用滚转角解算算法求出滚转角。
2.
By analyzing the layout of impulse thruster controllers, and the work process of laser detector and forces which acted on the trajectory correction projectiles, a impulse force control trajectory model on pitch plane was established.
研究了弹道修正弹末段脉冲推力控制的应用。
3.
This paper describes the basic principle of velocity pursuit guidance law and body pursuit guidance law of trajectory correction projectiles, researches the terminal correction trajectory and miss distance under pursuit guidance laws by 6—DOF trajectory simulation program, researches the orbit of laser detector ray axis and ground projection area of laser detector spatial viewpoint.
文中对速度追踪制导律和弹体追踪制导律的工作原理进行了研究,利用六自由度弹道仿真程序对弹道修正弹两种追踪方式下的末段修正弹道和脱靶量进行了对比计算,研究了两种追踪方式下激光探测器光轴的轨迹及激光探测器空间视场在地面投影区域的变化;弹体追踪方式命中精度虽然较低,但由于工程实现简单、成本低,仍有其工程使用价值。
6) trajectory correction
弹道修正
1.
To improve the concentration of projectiles,the one dimensional trajectory correctional projectile(TCP) with drag brake is researched.
为提高炮弹密集度,对采用阻力环装置的一维弹道修正弹进行了研究。
2.
For obtain muzzle velocity of projectile in the process of trajectory correction,a method for delermining muzzle velocity of projectile based on magnetoresistive sensor measuring muzzle velocity and acceleration was introduced.
在弹道修正过程中需要获知弹丸出炮口速度,提出采用磁阻传感器测量炮口速度和加速度信号判断弹丸到达炮口时速度的方法,给出了磁阻传感器信号输出、弹丸旋转频率以及炮口速度之间的解算式,对炮口测速装置进行了转台试验,得到了传感器输出信号与弹丸转速之间的波形曲线。
3.
Correction principle of trajectory correction projectile was analyzed.
分析了弹道修正弹的修正原理,针对某小口径高炮提出了一种弹道修正方案。
补充资料：整体壁板式弹体(见弹道导弹弹体)
整体壁板式弹体(见弹道导弹弹体)
monoblock wall-board missile body
zhengti bibanshi danti整体壁板式弹体(monobloek wall一board】二1551]e body)见弹道导弹弹体。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条