SYSTEM FOR CONTROL OF UNMANNED FLYING VEHICLE IN ROLL AND PITCH

摘要

FIELD: instrumentation engineering; onboard automatic control systems for flying vehicles of aeroplane configuration. ^ SUBSTANCE: proposed control system includes control process parameter setters, two multiplexers, two modulus detection units, two positive polarity signal detection units, two relay elements, two comparison units, two summing-up amplifiers, AND gate, controllable selector switch, four limiters, pitch and roll angle sensors, pitch and roll rate sensors, two adders and two actuating units. ^ EFFECT: enhanced accuracy of control due to combination method of guidance of unmanned flying vehicle. ^ 1 dwg