spin-stabilized missile

This paper takes a large slenderness ratio spin rocket with a low spin velocity for example, and the launch dynamic behavior of the system is investigated when there is a clearance between the missile and the launcher.

以大长径比低速旋转火箭为例，探讨弹-架间隙非线性特性对不同发射装置系统的动力响应的影响。

Next, analyses how the different spin angular velocity affects the motional steady-state magnitude and dynamic process of the spinning missile.

然后分析不同的自旋角速度对弹体运动的稳态性能和动态过程的影响。

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.

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；