FIELD: transport.
SUBSTANCE: proposed device comprises eleven adders, five amplifiers, two normally-open switches, five normally-closed switches, four integrators, two multipliers, spacecraft, flywheel engine, flywheel engine simulator, transducers of angular velocity and orientation angle, constant setter and memory. Signals of angular orientation and velocity are measured to generated spacecraft control signals, angular orientation estimation signals, those of angular velocity so that difference between appropriate signals and estimation signals is defined as well as those of spacecraft inertia and external interference estimation and for spacecraft orientation signal is corrected and generated.
EFFECT: higher accuracy and reliability.
2 cl, 1 dwg
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