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. Every of these channels contains sensor of angular position of aircraft and sensor of angular speed. 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, and outlet is connected with inlet of steering device drive with rigid feedback.
EFFECT: expansion of functional resources of device for control of angular motion of aircraft.
2 cl, 8 dwg
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