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。
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.
出处
《火力与指挥控制》
CSCD
北大核心
2010年第1期153-155,共3页
Fire Control & Command Control
关键词
空空导弹
越肩发射
变结构控制
反作用喷气
air-to-air missile ,over the shoulder ,variable structure control ,reaction jets control
