| 空空导弹越肩发射初制导转弯控制与仿真 |
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| 引用本文： | 雷震远,周军.空空导弹越肩发射初制导转弯控制与仿真[J].火力与指挥控制,2010,35(1). |
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| 作者姓名： | 雷震远 周军 |
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| 作者单位： | 西北工业大学,西安,710072 |
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| 摘 要： | 针对空空导弹越肩发射初制导俯仰平面180°转弯,提出了一种基于最优控制理论的最优转弯方法,该方法是确定一个最佳推力方向角,使转弯完成时导弹的末端速度最大。建立了简化的用于姿态控制的姿态动力学模型,采用反作用喷气控制系统(RCS)设计了导弹的姿态控制律。对空空导弹180°转弯的飞行过程进行了仿真并给出分析结果。
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| 关 键 词： | 空空导弹 越肩发射 变结构控制 反作用喷气 |
The Control and Simulation of Over the Shoulder of Air-to-Air Missile's Agile Turn |
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| LEI Zhen-yuan,ZHOU Jun.The Control and Simulation of Over the Shoulder of Air-to-Air Missile's Agile Turn[J].Fire Control & Command Control,2010,35(1). |
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| Authors: | LEI Zhen-yuan ZHOU Jun |
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| Abstract: | This paper describes the application of variable structure techniques to a longitudinal autopilot for an air-to-air missile performing a heading reversal maneuver.The dynamics was simplified for attitude control design.The control law was designed with reaction jets system.The simulations of a 180 degrees' turn of air-to-air missile were carried out, the results were given and analyzed. |
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| Keywords: | air-to-air missile over the shoulder variable structure control reaction jets control |
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