AIRCRAFT ADAPTIVE COORDINATED CONTROLLER Russian patent published in 2015 - IPC G05D1/00 G08G9/00 

Abstract RU 2554515 C1

FIELD: aircraft engineering.

SUBSTANCE: control device comprises bank transducer, bank angular velocity transducer, heading angle transducer, heading angular speed transducer, speed head transducer, first and second adding amplifiers, heading control signal master, first and second subtractors, inverting amplifier, first and second function nonlinear components with controlled limitation, nonlinear element with limitation and nonlinear element with non-sensitivity area and amplifier.

EFFECT: higher dynamic accuracy of control.

1 dwg

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Authors

Puchkov Aleksandr Mikhajlovich

Seleznev Anton Evgen'Evich

Khlopkin Artem Vladimirovich

Solov'Ev Aleksej Sergeevich

Dates

2015-06-27Published

2014-03-04Filed