1) corrected range
射程修正量
1.
Based on the calculational method, this paper also discusses calculational method for maximum corrected range.
基于射程扩展量的确定 ,也提出了最大射程修正量的计算方
2) range correction
射程修正
1.
The range correction ability of impulse force and body attitude while impulse forces not acting on the center of gravity was studied.
通过对弹上脉冲推力控制器布置、激光探测器工作过程和弹丸受力情况的分析,建立了俯仰平面内弹道修正弹末段脉冲推力控制的弹道模型,研究了脉冲推力的射程修正能力及非质心脉冲推力对弹体姿态的影响。
2.
The effect of range correction system of long-range rocket adopting SINS is analyzed through numerical simulation.
通过数值仿真的方法,研究了采用捷联惯导技术后远程火箭射程修正效果。
3.
A range correction for the attitude stabilized rocket is necessary.
射程修正的基础是对射程的准确预测 ,本文在弹道特征分析的基础上 ,提出了一些射程预测的方法 ,并采用蒙特卡洛仿真法研究了各种预测方法的精
3) 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。
4) range correction fuze
射程修正引信
1.
The method and precision of trajectory identification of a range correction fuze based on projectile of compound extended range by base bleed and rocket were studied.
研究了用于底排/火箭复合增程榴弹射程修正引信的弹道辨识方法以及辨识精度。
5) corrected flow ratio
修正引射流量比
6) elevation prediction correction
射角前置修正量
补充资料：射程
1.弹头射出后所能达到的距离。
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