SPEED CONTROL SYSTEM SPACECRAFT when approaching

摘要

The control system of spacecraft velocity during the approach, including a camera with a receiver on the basis of the CMOS sensor, characterized in that it introduced a narrowband filter, control unit and signal processing, disposed on the active spacecraft and four optical beacon on the passive spacecraft, wherein the optical beacons are located in the docking station plane perpendicular "OX" passive spacecraft axis, forming a rectangle with two sides parallel rows Sensitivity Yelnia CMOS sensor elements.