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Super-twisting sliding mode control for aircraft at high angle of attack based on finite-time extended state observer

Published Online: 2020-01-28

Published Print: 2020-03

Authors

Liu, Junjie

Sun, Mingwei

Chen, Zengqiang http://orcid.org/0000-0002-1415-4073
Sun, Qinglin
Funding

Funding for this research was provided by:

the National Natural Science Foundation of China (61973175, 61573197)

National Natural Science Foundation of China (61973172)

Key Technologies Research and Development Program of Tianji (19JCZDJC32800)
License Information

Text and Data Mining valid from 2020-01-28

Version of Record valid from 2020-01-28
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Article History

Received: 12 May 2019

Accepted: 10 January 2020

First Online: 28 January 2020

Compliance with ethical standards

:

: The authors declare that they have no conflict of interest.

: This article does not contain any studies with human participants or animals performed by any of the authors.

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