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专利要点本发明涉及一种导引自旋导弹沿着激光照射器(其可调光束限于导弹周围空域)的光轴飞行的光学控制系统。在采用这种系统时,对准照射器的导弹尾部有一个辐射接收机,它接收与导弹偏离照射器光轴的量相对应的信号,并有解调线路,此线路经一些偶合环节与能影响导弹弹道的操纵机构相连,并根据辐射接收机接收到的信号和能确定导弹滚动位置的基准信号产生偏差信号,以控制操纵机构。这种光
Patents The present invention relates to an optical control system that directs a spin-on missile to fly along the optical axis of a laser irradiator whose tunable beam is confined to the airspace surrounding the missile. In employing such a system, the rear of the missile aimed at the irradiator has a radiation receiver which receives the signal corresponding to the amount of the missile’s deflection from the optical axis of the illuminator and has a demodulation circuit which, via some coupling and energy Affect the ballistic missile control mechanism connected to and based on the signal received by the radiation receiver and can determine the missile rolling position of the reference signal deviation signal to control the operating mechanism. This light