A coupled nonlinear spacecraft attitude controller and observer with an unknown constant gyro bias and gyro noise
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Publication:5266691
DOI10.1109/TAC.2003.819289zbMath1364.93545OpenAlexW2154101061MaRDI QIDQ5266691
Publication date: 20 June 2017
Published in: IEEE Transactions on Automatic Control (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1109/tac.2003.819289
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