Attitude determination of a small satellite during plasma brake deorbiting experiment using an adaptive unscented Kalman filter during high angular velocity spin motion

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Original languageEnglish
Title of host publication6th European Conference for Aeronautics and Space Sciences (EUCASS 2015), Kraków, Poland, June 29 - July 3, 2015
Publication statusPublished - 2015
MoE publication typeD3 Professional conference proceedings

ID: 1972243