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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
Abstract:
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.
Keywords:
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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