FIELD: physics.
SUBSTANCE: invention is related to the field of instrument making and may be used for control of angular motion of aircrafts. Method provides formation of optimal indices of transition processes by coordinates of angular motion of aircraft. At that control of aircraft is carried out without correction of proportionality coefficients of control laws of angular motion of aircraft in full operation range of changes of velocities and altitudes of flight, and also for channel of pitch and during change of aircraft alignment in the process of motion.
EFFECT: expansion of functional resources of device for control of angular motion of aircrafts.
6 dwg
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