1) rolling missile
滚转导弹
1.
The paper then applies the above mentioned decoupling control theory in the decoupling guidance design of rolling missiles.
本文将该理论用于滚转导弹解耦制导的设计中 ,数字仿真表明所设计的制导系统不仅精度高 ,而且具有鲁棒性。
2.
The mechanism of dynamic instability of rolling missile was analyzed by describing the dynamics of rolling missile as a closed loop with dynamic negative feedback.
将滚转导弹动力学系统描述为一个具有动态负反馈的闭环系统,分析了滚转导弹动态失稳的机理。
2) rolling missile
滚转弹
1.
Estimation of the attitude of a rolling missile based on independent component analysis;
一种基于独立成分分析的滚转弹姿态解算
2.
A scheme to estimate the flight attitude of a rolling missile based on strong tracking filter(STF) was proposed.
给出一种基于强跟踪滤波器(STF)的滚转弹飞行姿态获取方法。
3) derivative in roll
滚转导数
4) self-induced spin
自诱导滚转
5) rolling missile
旋转导弹
1.
In order to avoid cross couplings between the vertical and lateral motion,decoupling control of a double-channel control rolling missile autopilot was studied.
为消除旋转导弹自旋所带来的纵向与侧向运动的交叉耦合,进行了双通道控制旋转导弹自动驾驶仪回路解耦控制研究。
2.
Based on the characteristics of rolling missile with double-channel control,the autopilot loop is transferred from body coordinate system to quasi-body coordinate system after a rolling transfer.
根据双通道控制旋转导弹的特点,通过旋转变换,将弹体坐标系下的自动驾驶仪回路变换到准弹体坐标系下,并比较了与倾斜稳定导弹标准自动驾驶仪的区别。
3.
The analysis of the character, principle, and realization for the guidance technology of rolling missile is made.
分析了旋转导弹制导技术的特点、原理、实现方法 ;结合典型型号 ,对旋转导弹制导技术的应用进行了综述 ;并对其发展方向进行了预测。
6) rotating missile
旋转导弹
1.
A moving mass control of rotating missile is a kind of new control mode,it differs from other control modes because it generates an angle of attack and an angle of sideslip directly from the mass motion.
针对导弹变质心这种新的控制方式,建立了变质心旋转导弹准弹体下的动力学模型,由于模型是复杂非线性的,通过按线性化族近似化理论对模型进行了合理简化,并用动态逆控制理论对系统的姿态控制进行了设计,仿真结果表明,所设计的变质心导弹动态逆姿态控制具有很好的快速性、稳定性。
2.
Trajectory simulation of rotating missile is the basis of optimization designs for fins of missile and trajectory.
旋转导弹弹道仿真是弹翼结构优化设计和弹道优化设计的基础。
补充资料：滚转
1.滚动;转动。
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