Missile control in the polar coordinate system using a scalar radius

Missile control in the polar coordinate system using a scalar radius
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使用标量半径在极坐标系中进行导弹控制

DOI：
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发表时间：
2015
期刊：
影响因子：
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通讯作者：
A. F. Indyukhin
A. F. Indyukhin
中科院分区：
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文献类型：
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作者：
V. N. Khruslov;S. Feofilov;O. V. Goryachev;I. M. Lavit;A. F. Indyukhin

文献摘要

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提出了一种极坐标系下的无陀螺导弹控制方法。研究了质点在控制力作用下的运动。所有的系统组件的频率特性进行了计算。已选择校正滤波器。确定了控制系统的稳定裕度和传递系数。进行了数学模拟。获得了导弹的飞行轨迹。
A method for gyroless missile control in the polar coordinate system is proposed. Motion of a material point under control force is studied. Frequency characteristics of all of the system components have been calculated. A correction filter has been chosen. Stability margin and the transfer coefficient of the control system have been determined. Mathematical simulation has been carried out. The missile flight trajectorys have been obtained.