FIELD: spacecraft attitude control in performing manoeuvres is space; objects located in support-free space. SUBSTANCE: method consists in mounting twin circular electromagnetic balancers inside housing of object and adjusting the rotational speeds of circular rotors of electromagnetic balancers independently for each balancer in pair. Twin electromagnetic balancers are mounted at ends of object housing (at end faces and at side) along longitudinal and transversal axes of object; planes of electromagnetic balancers are oriented perpendicularly to these axes. EFFECT: simplified construction and improved functional and arrangement properties. 3 cl, 3 dwg
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