FIELD: rocket engineering, rocket controlling. SUBSTANCE: coordinates of target and rocket are found in sequence when rocket is controlled. Ground equipment generates control command signals which are sent to board rocket. Transmission of control commands to rocket over time of rocket flight equal to 0.5-3.0 s and covering moment of separation of stages is conducted under mode of limitation of signals by amplitude. Level of limitation is chosen within bounds from 25 to 80% of full working range of amplitude of signals of control commands. EFFECT: enhanced reliability of method. 2 dwg
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