"Twistors-Based Attitude-Orbit Integrated Control for Spacecraft: A ..."

Dongyan Jin et al. (2025)

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DOI: 10.1109/TSMC.2024.3519436

access: closed

type: Journal Article

metadata version: 2025-03-07

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Dongyan Jin, Yannan Bi, Tong Wang, Jianbin Qiu, Huijun Gao:
Twistors-Based Attitude-Orbit Integrated Control for Spacecraft: A High-Order Fully Actuated System Approach. IEEE Trans. Syst. Man Cybern. Syst. 55(3): 2098-2105 (2025)

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