FIELD: physics.
SUBSTANCE: invention is related to the field of instrument making and may be used for control of angular motion of aircrafts. System of aircraft angular motion control contains channels of snaking, list and pitch. Every of these channels contains sensor of angular position of aircraft, sensor of angular speed and sensor of angular acceleration. At that the first inlet of the first summary amplifier is connected to sensor of angular position of aircraft, the second inlet is connected to sensor of angular speed, the third inverting inlet is connected to outlet of setter of required value of angular position of aircraft, the fourth inlet is connected to outlet of angular acceleration sensor, and outlet is connected with inlet of steering device integrating drive.
EFFECT: expansion of functional resources of device for control of angular motion of aircrafts.
2 cl, 6 dwg
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