Crossmark

Robust $$H_\infty $$ H ∞ output feedback control for attitude stabilization of a flexible spacecraft

Crossref DOI link: https://doi.org/10.1007/s11071-016-2624-5

Published Online: 2016-01-29

Published Print: 2016-04

Update policy: https://doi.org/10.1007/springer_crossmark_policy

Authors

Wu, Shunan https://orcid.org/0000-0001-6273-6425
Wen, Shenghui
Funding

Funding for this research was provided by:

National Natural Science Foundation of China (11502040)

Education Department of Liaoning Province (L2014030)

Fundamental Research Funds for the Central Universities (DUT15LK31)
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Text and Data Mining valid from 2016-01-29