Spacecraft output feedback attitude control based on extended state observer and adaptive dynamic programming

Li-Gang Gong, Qing Wang, Chaoyang Dong. Spacecraft output feedback attitude control based on extended state observer and adaptive dynamic programming. J. Franklin Institute, 356(10):4971-5000, 2019. [doi]

Authors

Li-Gang Gong

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Qing Wang

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Chaoyang Dong

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