1.
This paper introduces a method to analysis coupling of rolling missile.
研究了一种对滚转导弹进行耦合性分析的方法。
2.
Design on stabilization loop of roll-isolated SINS in spinning projectile
旋转弹用横滚隔离捷联惯导稳定回路设计
3.
Design of Mixed Sensitivity Robust Controller for the Roll-Channel of the Guided Bomb
制导炸弹滚转通道混合灵敏度鲁棒控制器设计
4.
Numerical Research of Rolling Characteristics on Canard Missiles by Distance between Fin and Wing
鸭式导弹舵翼面间距影响滚转的数值研究
5.
In the absence of sophistication the missile will roll through 340°.
不完善时导弹应滚动340°．
6.
Design of Roll Control Based on Parameter Space Method for Guided Bomb with SINS/GPS
基于参数空间法的SINS/GPS制导炸弹滚转控制器设计
7.
Research of Dynamic and Control of Spinning Ballistic Missile;
弹道导弹滚动飞行动力学与控制研究
8.
The Performance Analysis of the Antiroli Torsion Bar Spring Installed in High Speed Bogie
高速转向架抗侧滚扭杆弹簧性能分析
9.
India s Ballistic Missile Program and Transformation of Missile Nonproliferation Policy;
印度的弹道导弹计划和导弹防扩散政策的转变
10.
The missiles were moved under convoy.
导弹在护卫之下转移.
11.
Research and Development the Emulation Turntable of Control Rolling and Transferring for Missile;
弹箭滚转控制仿真实验台的设计与实现
12.
Influence of Rotation on Relative Orientation Between Projectile and Target Measured by CCD
滚转对用CCD组合测量弹目相对方位的影响
13.
How to reduce the tactical missile hull straightness error produced in forming by the bender with three rollers is a difficult problem for the missile hull manufacturing technique.
如何减小战术导弹外壳板(简称弹壳板)滚弯直线度误差是目前导弹生产工艺中的难题.
14.
The other is the miniature ball bearing, essential in the assembling of a missile-guidance system.
另一件是微型滚珠轴承，这是装配导弹的制导系统所必不可少的。
15.
Vibration Characteristics of Jeffcott Rotor System Supported by Cylindrical Roller Bearings
圆柱滚子轴承若干参数对弹性转子系统临界转速的影响
16.
Design of Guidance and Control of Air-Launched BTT Missile
空射倾斜转弯导弹制导控制系统设计
17.
Stiffness Calculation for Linear Rolling Guide with Elastic Deformation of Slide Block Taken into Account
直线滚动导轨考虑滑块体弹性变形时的刚度计算
18.
The Development of Dynamic Measuring Instrument for Checking Lead Errors of Ball Screws of Steering Mechanism
转向器滚珠丝杆导程误差动态检测仪的研究