FIELD: physics; navigation.;SUBSTANCE: invention relates to designing navigation systems and can be used for controlling asynchronous motors of powered gyrostabilisers with variable kinetic momentum, particularly used in positioning systems of artificial earth satellites (AES). To achieve the given result, the degree of functional connections for each control channel can be separately established before operating the control system and directly during processing, for example each "step" of program-reference-input signals. The above mentioned functionalities in many practically important cases of program control of electric drives of artificial earth satellite gyrostabilisers, from the view point of simplifying the process of setting up and optimising control modes (smoothness of transient processes during launch due to reduction of intensity of electromagnetic processes), give the proposed system an edge over existing engineering solutions.;EFFECT: increase in main quality factors of processing program-reference-input signals in a wide range of destabilising effects on artificial earth satellites, and more specifically speed of operation and accuracy through passive setup (adaptation) of each gyrostabiliser control channel.;4 dwg
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