FIELD: aircraft control systems.
SUBSTANCE: inventions group relates to aircraft stabilization and control system (options), aircraft stabilization and control method, aircraft (options). The system according to the first version contains a housing, two elements, an adder, two pistons, a control device, an adjustable limiting device, a threaded head. The method includes steps for the interaction of the above elements of the system. The system according to the second version, unlike the first one, additionally contains a second control unit and a backup control unit. Each of the variants of the aircraft contains a flight control system, at least one: a control element, a controlled element, an actuator, a system for increasing stability and control according to the corresponding variant.
EFFECT: increased stability and strengthening of commands for controlling the aircraft.
28 cl, 3 dwg
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Authors
Dates
2022-04-25—Published
2018-10-05—Filed