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  • Onboard Two-Step Attitude D...
    Kramlikh, A. V.; Nikolaev, P. N.; Rylko, D. V.

    Gyroscopy and navigation (Online), 06/2023, Letnik: 14, Številka: 2
    Journal Article

    The paper describes the measuring aids (magnetometers and light sensors) and attitude determination algorithms of SamSat-ION nanosatellite. The Kalman filter based on magnetometer measurements only is used as a basic algorithm, and the auxiliary QUEST algorithm provides a priori estimation of the quaternion input to the Kalman filter. The two-step algorithm simulation has been performed, and its efficiency has been verified.