FIELD: on-board control complexes for navigation, indication and control of flying vehicles. SUBSTANCE: proposed complex includes system of flight parameter sensors and integrated system of radio navigation and radio communication which are connected in parallel with display system and director-control system computer which is connected with display system. Proposed complex includes also auto-pilot with actuators of limited stroke. Auto-pilot is connected with system of flight parameter sensors at input and with combined unit of helicopter control system at output. Complex is additionally provided with trajectory control computer whose inputs of direct communication are connected to outputs of director-control computer and to system of flight parameter sensors and outputs are connected to inputs of pitching, rolling, direction and collective pitch channels. EFFECT: enhanced efficiency. 2 cl, 1 dwg
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Authors
Dates
2003-12-27—Published
2002-10-18—Filed