METHOD OF FORMING A CONTROL SIGNAL OF A STEERING DRIVE OF AN UNCLEANED AIRCRAFT AND A DEVICE FOR ITS IMPLEMENTATION Russian patent published in 2019 - IPC B64C13/00 G05D1/00 G05B11/14 

Abstract RU 2681823 C1

FIELD: physics; aviation.

SUBSTANCE: group of inventions relates to a method and device for generating a steering signal control signal of an unmanned aerial vehicle (UAV). To generate a control signal, they set a control signal, amplify it and limit it, filter the subtraction signal, amplify the filtered signal, form the current speed signal deflection steering and scale it, work out the current signal deflection steering actuator, while additionally measure the velocity head, angle of attack, coefficient of efficiency of the hinge moment from the angle of attack and from the rudder deviation, form the current speed signal taking into account its insensitivity in the zone of the current value of the hinge moment in a certain way. Device contains a control signal adjuster, two signal amplifiers, a signal limiter, two subtraction elements, an inertial filter, an actuator and an actuator, a deflection angle signal sensor, a deflection speed signal sensor, an inertial amplifier, sensors of velocity head and angle of attack, sets of efficiency factor for articulated torque from steering deflection and angle of attack, two multipliers, summing amplifier, amplifier with non-sensibility zone, connected in a certain way.

EFFECT: provides enhanced functionality and improved control accuracy of the UAV.

2 cl, 1 dwg

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RU 2 681 823 C1

Authors

Syrov Anatolij Sergeevich

Kedrova Nadezhda Nikolaevna

Puchkov Aleksandr Mikhajlovich

Petrov Andrej Borisovich

Sukhova Valeriya Lvovna

Tatsyuk Dmitrij Grigorevich

Khlopkin Artem Vladimirovich

Dates

2019-03-12Published

2018-06-26Filed