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.

This article is cited 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.

DOI: 10.20948/prepr-2017-126