摘要
介绍了用简化红外导弹运动学和动力学模型的方法,对导弹的方位和俯仰二个制导系统作单独的仿真检测,介绍了仿真系统的原理及所需设备。可以从计算机屏幕上作图,以判断检测结果。
This paper introduces the method of infrared missile simulation testin bearing and pitching channel guide system with the simplified kinematics anddynamics models.It also presents the principle of simulation system and equipmentrequired.his system can make the figure in the computer CRT.and determine thetesting result.
出处
《火力与指挥控制》
CSCD
北大核心
1993年第2期77-80,共4页
Fire Control & Command Control
关键词
导弹
制导
检测
仿真
angle of course
angle of track
average pneumatic string
