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Reduced-Order Sliding Mode Observer-Based Backstepping Integral Logarithmic Sliding Mode Control: Application to Wing Aeroelastic System

Published Online: 2024-10-14

Published Print: 2025-03

Authors

Mahmood, Ahmad https://orcid.org/0000-0002-4348-6501
ur Rehman, Fazal

Okasha, Mohamed
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Text and Data Mining valid from 2024-10-14

Version of Record valid from 2024-10-14
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Article History

Received: 10 February 2024

Revised: 2 April 2024

Accepted: 19 September 2024

First Online: 14 October 2024

Declarations

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: The author(s) declare that they have no competing financial interests or personal relationships that could appear to influence the work reported in this paper.

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