摘要
以垂直发射的反坦克导弹为研究对象,介绍了国内外在垂直起飞-快速转弯、全方位发射以及制导律等若干关键技术方面的研究现状,指出了气动力/推力矢量复合控制技术是解决快速转弯的有效策略,空中自主完成全方位快速转弯是全方位发射的关键。以比例导引为基础的滑模变结构多条件约束制导律是反坦克导弹制导控制的研究方向,分析了反坦克导弹滚转飞行、大攻角飞行过程中存在的问题并提出了解决方案。
The research status of some key technologies, such as take-off/quick turn, all-directions launch and guidance law for vertical launched anti-tank missiles are introduced at home and aboard. It is pointed out that the hybrid control technology of aerodynamic/thrust vector control is an effective method to solve the problem of quick turn. Quick turn with full angles in the air is the key to all-directions launch. The sliding mode constraint guidance law with multi conditions based on proportional guidance is the research direction of anti-tank missile guidance and control. The existing problems of roll flight and large attack-angle in the process of anti-tank missile fighting are analyzed and several solutions are proposed.
出处
《战术导弹技术》
北大核心
2016年第3期77-82,100,共7页
Tactical Missile Technology
关键词
反坦克导弹
垂直发射
全方位
制导律
anti-tank missile
vertical launch
all-directions
guidance law
