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KIAM Preprint № 64, Moscow, 2014
Authors: Ivanov D. S., Ivlev N. A., Karpenko S.O., Ovchinnikov M. Y.
Attitude determination algorithms investigation for microsatellites of 'TabletSat' series
Attitude determination algorithms based on Kalman filter are considered in the paper. The algorithms processes measurements of a star sensor, gyro, magnetometer and sun sensor. Quaternion and angular velocity vector are choosen as a state vector, and for a several algorithms also biases of magnetometer and gyro measurements are also estimated. The algorithms are investigated with parameters of the 'TabletSat-Aurora' microsatellite.
microsatellite attitude determination, Kalman filter
Publication language: russian,  страниц: 24
Research direction:
Theoretical and applied problems of mechanics
Russian source text:
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