FIELD: aviation.
SUBSTANCE: aircraft automated control system in the longitudinal channel during refuelling in the air comprises a static remote control system (RCS) signal computer, a stabilizer (elevator) steering drive, a stabilizer (elevator), pitch control stick position sensor, pitch angular speed sensor, angle of attack sensor, normal overload sensor, pitch angle sensor, roll angle sensor, unit for generating switching signals by commands from the pilot, five signal switching units, normal overload processing circuit signal computer, preset overload signal computer when aircraft approaches tanker, preset overload signal calculator during positional control, four signal amplifiers, seven adders, integrator, input signal change rate limiting unit, unit of constant single signal, five non-linear units, three memory devices, calculator of angle of inclination of flight trajectory of aircraft, computer of correcting signal of overload, which are connected in a certain manner.
EFFECT: higher accuracy and safety.
4 cl, 6 dwg, 2 tbl
Title | Year | Author | Number |
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RU2769452C1 |
REMOTE REDUNDANT SYSTEM OF AUTOMATED MODAL CONTROL IN LONGITUDINAL CHANNEL OF MANEUVERED MANNED AND UNMANNED AIRCRAFTS | 2015 |
|
RU2645589C2 |
METHOD OF AIRCRAFT CONTROL IN LANDING APPROACH | 2012 |
|
RU2537201C2 |
Authors
Dates
2025-01-28—Published
2022-08-03—Filed