METHOD FOR GENERATING OF FLYING AIRCRAFT ANGULAR MOTION ADAPTIVE CONTROL SIGNAL Russian patent published in 2008 - IPC G05D1/08 

Abstract RU 2338235 C1

FIELD: instrument making.

SUBSTANCE: method comprises following operations, i.e. measurement of current angular position and angular speed signals, generation of angular position reference signal, generation of signal of mismatch between the angular position preset and current signals. The method includes also generating the control signal equal to the sum of the mismatch and angular speed signal components to initiate actuator, measuring kinetic head signal and generating adaptive signal be proportional scaling the kinetic head signal.

EFFECT: invariance of stabilisation quality and increased control accuracy.

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RU 2 338 235 C1

Authors

Syrov Anatolij Sergeevich

Puchkov Aleksandr Mikhajlovich

Dates

2008-11-10Published

2007-04-27Filed