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This article is cited in 1 scientific paper (total in 1 paper)
Attitude motion of the TNS-0 №2 nanosatellite
D. S. Ivanov, M. Yu. Ovchinnikov, O. A. Pantsyrnyi, A. S. Selivanov, I. O. Fedorov, O. E. Khromov, N. A. Yudanov
Abstract:
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.
Keywords:
nanosatellite, attitude motion, magnetometer, sun sensor.
Citation:
D. S. Ivanov, M. Yu. Ovchinnikov, O. A. Pantsyrnyi, A. S. Selivanov, I. O. Fedorov, O. E. Khromov, N. A. Yudanov, “Attitude motion of the TNS-0 №2 nanosatellite”, Keldysh Institute preprints, 2017, 126, 27 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp2342 https://www.mathnet.ru/eng/ipmp/y2017/p126
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