METHOD FOR GENERATING OF FLYING AIRCRAFT ANGULAR MOTION ADAPTIVE CONTROL SIGNAL

METHOD FOR GENERATING OF FLYING AIRCRAFT ANGULAR MOTION ADAPTIVE CONTROL SIGNAL

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...

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Bibliographische Detailangaben
Hauptverfasser: PUCHKOV ALEKSANDR MIKHAJLOVICH, SYROV ANATOLIJ SERGEEVICH
Format: Patent
Sprache:eng ; rus
Schlagworte:
CONTROLLING
PHYSICS
REGULATING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
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Beschreibung
Zusammenfassung: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.