1) 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。
2) ballistic correction
弹道修正
1.
Base on the theory that additional control force come from nose angle,the feasibility of performing one dimen- sion ballistic correction by eontroUing rocket nose sngle is researched,and the main factor affecting correction capacity is analyzed via modeling.
基于控制头部偏角来产生附加控制力的思想,进行了控制弹箭弹头部偏角实现一维弹道修正的可行性研究,并建模分析了影响修正弹修正量的主要因素。
2.
This thesis dicusses the detailed concepts of realizing two-dimensional ballistic correction on simple control technology of trajectory.
通过对弹道修正弹在脉冲修正力作用下的受力分析，建立了简易控制二维弹道修正弹一般形式下的六自由度有控弹道方程，并针对弹道修正的具体模式分析了其具体的控制方程。
4) 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。
5) 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。
6) 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。
补充资料：弹道(见弹道学)
弹道(见弹道学)
trajectory
dQfldQO弹道(t rajectory)见弹道学。
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