1) 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。
2) High-speed Rotary Missile
高速旋转弹
1.
Research on Attitude Measurement of High-speed Rotary Missile;
高速旋转弹姿态参数测试技术研究
2.
In view of the high speed spinning and the small caliber of High-speed Rotary Missile, the small diameter non-gyro posture parameter test system is designed, and the attitude parameter of missile aviation is tested and stored.
本文针对高速旋转弹高速自旋的特点和小口径的测试要求,设计了无陀螺的小直径姿态参数测试系统,实现了弹体飞行全过程姿态参数的测试及存储。
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。
5) 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。
6) 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。
补充资料：高速
高速度；～发展│～公路。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
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