1) missile spin
弹体自旋
1.
Methods The number of rosette scan petals required for the instantaneous FOV to cover the total FOV was calculated and the effects of the gyro rotational frequency, motor rotational frequency and missile spin rate variations on rosette scan patterns and frame frequencies were predicted.
目的 探讨将玫瑰扫描红外导引头应用于自旋弹的可行性； 方法 通过研究陀螺、空心电机转动频率变化及弹体自旋条件下瞬时视场覆盖全视场所需的玫瑰花瓣数，得出上述三者对玫瑰扫描空间图案和不漏扫帧频的影响； 结果与结论 在弹上增加自旋频率测量装置并对陀螺及空心电机转动频率有负反馈稳速控制的条件下，红外玫瑰扫描导引头可以应用于自旋弹
2) 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。
3) 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。
4) spinning warhead
自旋弹头
1.
At last,simulation about the three-axis warhead and spinning warhead was conducted and the results validate the feasibility of mass moment control.
5/Simulink环境下,设计开发了六自由度导弹仿真系统,并且针对三轴稳定弹头和自旋弹头进行数值仿真,仿真结果验证了质量矩控制的有效性。
2.
The varying centroid control system was studied,by which a spinning warhead realizing the terminal maneuvering.
对自旋弹头实现末端机动的变质心控制系统进行了研究。
3.
In order to express clearly and directly the relationship between controlled variables and attitude motion of a spinning warhead,the Newton dynamics method is applied to construct its attitude motion model.
为了明确直观地表现自旋弹头姿态运动与控制量之间的关系,采用牛顿力学方法建立了自旋弹头的姿态运动模型。
5) missile spinning
导弹自旋
补充资料：半硬壳式弹体(见弹道导弹弹体)
半硬壳式弹体(见弹道导弹弹体)
semi-hard-shelled missile body
bQn yingkeshi dan桩半硬壳式弹体(semi一hard一shelled、ssilebody)见弹道导弹弹体。
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