SYSTEM OF CONTROL OF ANGULAR MOTION OF AIRCRAFT WITH STATIC DRIVE

摘要

FIELD: physics. ^ SUBSTANCE: invention is related to the field of instrument making and may be used for control of angular motion of aircrafts. Control system contains channels of snaking, list and pitch. At that suggested method provides optimal indices of transition processes by coordinates 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 aircraft ^ 8 dwg