FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to remote control system. Remote control system comprises two connection cabinets 1, each housing two identical computers 3 to support: algorithms to generate required positions of all airfoils in automatic and manual control, algorithms to control solenoid valves of hydroelectric drives, algorithms of automatic control, and algorithms to generate margin magnitude of individual parameters of flight. Said cabinets 1 houses power supplies 3 with their voltage outputs connected to inputs of computer s 3 and power amplifiers 5. Inputs of the latter are connected to computer outputs. Power amplifier outputs are connected via said cabinet and aircraft cable system to inputs of servo drives of stabilisers 7, nose flaps 8, differential flaps 9, rudders 10, and engine rotary nozzles 11.
EFFECT: decrease weight and sizes, perfected control of primary airfoils.
4 cl, 7 dwg
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Authors
Dates
2013-01-20—Published
2011-06-23—Filed