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"Adaptive Reduced Attitude Control for Rigid Spacecraft With Elliptical ..."

Yueyang Liu, Qinglei Hu, Gang Feng (2023)

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DOI: 10.1109/TAES.2022.3232319

access: closed

type: Journal Article

metadata version: 2023-08-18

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Yueyang Liu, Qinglei Hu, Gang Feng:
Adaptive Reduced Attitude Control for Rigid Spacecraft With Elliptical Pointing Constraints. IEEE Trans. Aerosp. Electron. Syst. 59(4): 3835-3847 (2023)

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