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KIAM Preprint № 126, Moscow, 2017
Authors: Ivanov D. S., Ovchinnikov M.Y., Pantsyrnyi O.A., Selivanov A.S., Fedorov I.O., Khromov O.E., Yudanov N.A.
Attitude motion of the TNS-0 №2 nanosatellite
A passive attitude motion of the TNS-0 №2 nanosatellite is determined using magnetometer and sun sensor measurements. Time of initial angular motion damping is estimated. The accuracy of the magnetic stabilization is studied.
nanosatellite, attitude motion, magnetometer, sun sensor
Publication language: russian,  страниц: 27
Research direction:
Theoretical and applied problems of mechanics
Russian source text:
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