The invention relates to an
infrared touch screen hardware circuit of an instrument
system of a manned
spacecraft, which is suitable for the
aerospace field. The hardware circuit of the touch screen is composed of the basic working circuit of the
infrared pair tube, the horizontal emitting tube lamp array and
control circuit, the horizontal
infrared receiving tube circuit, and the current output circuit. It can work stably and reliably under high and low temperature and vacuum conditions, and meets the special
aerospace environment. Use the following requirements. The circuit structure is simple, the volume is small, the reliability is high, the work efficiency is improved, and the
power loss is reduced.