METHOD OF GENERATING SIGNAL TO CONTROL AIRCRAFT ANGULAR FLIGHT AND DEVICE TO THIS END Russian patent published in 2013 - IPC G05D1/00 

Abstract RU 2490686 C1

FIELD: aircraft engineering.

SUBSTANCE: control signal generator comprises control signal selector 1, comparator 2, fist amplifier 3, adder 4, filter 5, signal clipper 6, angle transducer 7, angular velocity transducer 8, second amplifier 9, velocity head transducer 10, logical comparator 11, controlled switch 12, third amplifier 13 and critical velocity head selector 14.

EFFECT: expanded operating performances owing to use of velocity head parameter and higher dynamic accuracy of drone control.

2 cl, 1 dwg

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RU 2 490 686 C1

Authors

Syrov Anatolij Sergeevich

Zhdanovich Nadezhda Pavlovna

Kravchuk Sergej Valentinovich

Ogol'Tsov Igor' Ivanovich

Popov Boris Nikolaevich

Puchkov Aleksandr Mikhajlovich

Solov'Ev Aleksej Sergeevich

Dates

2013-08-20Published

2012-06-05Filed