FIELD: aviation; autopilot technologies.
SUBSTANCE: autopilot of a highly maneuverable aircraft, containing a block for generating control commands and a block for processing commands for controlling and stabilizing the rocket relative to three axes of the associated coordinate system. The unit for processing control and stabilization commands is configured to generate control commands to the steering gears of the aircraft for testing the flight trajectory based on one of the reference trajectories formed by the onboard computer.
EFFECT: possibility of transferring the entire aircraft motion control system to a digital basis is achieved.
1 cl, 4 dwg, 1 tbl
