1) high spinning projectile
高自旋弹丸
1.
A method of solving the angular speed and attitude angular of high spinning projectile was proposed by accelerometers\' specific force signal in existence of installation errors.
研究了存在安装误差时基于加速度计比力信号解算高自旋弹丸角速度和姿态角的方法。
2) high-speed rotating projectile
高速旋转弹丸
1.
It is very difficult to make trajectory correction for high-speed rotating projectile because of rotating characteristic,which can not be solved by adopting the traditional correction projects.
解决由于高速旋转弹丸的旋转特性导致难以采用常规方案对其进行弹道修正的技术难点。
3) spinning projectile
旋转弹丸
1.
It is desired during spinning projectile and missile design and trajectory calculation that the side force and moment, Magnus force and moment, must be predicted precisely.
旋转弹丸、导弹的设计和弹道计算都要求准确计算弹丸的侧向力、力矩-马格努斯力、力矩。
4) high-velocity projectile
高速弹丸
1.
This paper has reviewed the present development of the high-velocity projectiles abroad.
综述了目前高速弹丸的研制状况,主要对电磁炮发射的高速弹丸有关技术问题作了较详细的综述,并述及了高速弹丸的发展趋势。
5) self-rotating spring
自旋弹簧
1.
Geometric parameters of the self-rotating spring may greatly affect the heat transfer and automatic fouling-remove in the heat transfer tubes.
换热管内插自旋弹簧的几何参数对其强化传热和自动除垢效果有重要的影响,通过对多组试验结果的比较分析,得出了无量纲参数D1/S、D1/D0对换热管内自旋弹簧的转动特性和流体阻力特性的影响规律,并在大量试验数据的基础上归纳出一个换热管内自旋弹簧工作性能的综合评判准则——L z准数。
6) Spinning Missile
自旋导弹
1.
Magnetic Sensor Application in IMU of Spinning Missile;
地磁传感器在自旋导弹惯测组合中的应用研究
2.
Study of periodic equivalent control force of spinning missile;
自旋导弹周期等效控制力的研究
3.
Direction error is one of the special problems during the guidance of spinning missiles.
方位误差是自旋导弹自动导引过程中较特殊的问题。
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