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Systematic fuzzy Navier–Stokes equations for aerospace vehicles

ZY Chen (Guangdong University of Petrochem Technology, School of Science, Maoming, PR China)
Yahui Meng (Guangdong University of Petrochem Technology, School of Science, Maoming, PR China)
Ruei-Yuan Wang (Guangdong University of Petrochem Technology, School of Science, Maoming, PR China)
Timothy Chen (Division of Engineering and Applied Science, California Institute of Technology, Pasadena, CA, USA)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 27 January 2022

Issue publication date: 10 February 2022

135

Abstract

Purpose

To prove the effectiveness of the proposed design method, this study aims to propose the Fisher equation and temperature cooling fins that control high-speed aerospace vehicles.

Design/methodology/approach

A new approach whereby the control of aerospace vehicles can be achieved by fuzzy controller and appropriate Navier–Stokes equations in this article. The design of the controller based on models of Navier–Stokes equations simplified complex mathematical simulations and approximations.

Findings

If the fuzzy controller cannot stabilize the system, the Navier–Stokes fuzzy function is injected into the system as a controller tool, and the system is asymptotically stabilized by adjusting the fuzzy parameters.

Originality/value

The simulation results show that if the tuning frequency is high enough, the fuzzy controller and fuzzy observer can create chaotic movements by adjusting the dither amplitude appropriately. The demonstration of the Fisher equation and the temperature-cooled fin control problem for high-speed aerospace vehicles has displayed the benefits of combining fuzzy control with the Navier–Stokes equation.

Keywords

Acknowledgements

The authors are grateful for the research grants given to Yahui Meng from the Provincial key platforms and major scientific research projects of universities in Guangdong Province, Peoples R China under Grant No. 2017GXJK116, and the research grants given to ZY Chen from the Projects of Talents Recruitment of GDUPT (NO. 2021rc002) in Guangdong Province, Peoples R China No. 2021rc002 as well as to the anonymous reviewers for constructive suggestions.

The publishers of Aircraft Engineering and Aerospace Technology wish to retract the article “Systematic fuzzy Navier-Stokes equations for aerospace vehicles” by Z. Chen, Y. Meng, R.Y. Wang, and T. Chen, which appeared in Volume 94, Issue 3, 2022.

It has come to our attention that there are concerns regarding the affiliations of the authors and the originality of the paper. A reasonable description of authors’ contribution to the paper has not been provided and concerns regarding their affiliations have not been addressed. An investigation has shown evidence of a compromised peer review process. As a result, the findings of the article cannot be relied upon.

Authors submitting to the journal are expected to adhere to the guidelines and policies of the journal.

The publishers of the journal sincerely apologize to the readers.

Citation

Chen, Z., Meng, Y., Wang, R.-Y. and Chen, T. (2022), "Systematic fuzzy Navier–Stokes equations for aerospace vehicles", Aircraft Engineering and Aerospace Technology, Vol. 94 No. 3, pp. 351-359. https://doi.org/10.1108/AEAT-06-2020-0109

Publisher

:

Emerald Publishing Limited

Copyright © 2021, Emerald Publishing Limited

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