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"Continuous Finite-Time Attitude Control for Rigid Spacecraft Based on ..."

Qinglei Hu, Boyan Jiang (2018)

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DOI: 10.1109/TAES.2017.2773340

access: closed

type: Journal Article

metadata version: 2020-04-16

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Qinglei Hu, Boyan Jiang:
Continuous Finite-Time Attitude Control for Rigid Spacecraft Based on Angular Velocity Observer. IEEE Trans. Aerosp. Electron. Syst. 54(3): 1082-1092 (2018)

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