This work presents a general approach to the problem of safe aircraft landing on a moving platform. Parameters needed to be monitored during the landing were listed. The problem of optoelectronic systems in control of the position of the landing field was formulated. The structure of the measuring system was reviewed, and listed the options and features of each of its elements. There was proved the necessity of calibration TV camera, which is the component of the receiver optoelectronic system. The method of calibration of one of its main parameters was proposed. In conclusion, directions for further research are presented. One of the main areas is the study of the nature of the measurement error and its evaluation.