Continuous Finite-Time Attitude Control for Rigid Spacecraft Based on Angular Velocity Observer

Qinglei Hu, Boyan Jiang. Continuous Finite-Time Attitude Control for Rigid Spacecraft Based on Angular Velocity Observer. IEEE Trans. Aerospace and Electronic Systems, 54(3):1082-1092, 2018. [doi]

Authors

Qinglei Hu

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Boyan Jiang

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