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Coupled Systems Mechanics Volume 12, Number 3, June 2023 , pages 221-239 DOI: https://doi.org/10.12989/csm.2023.12.3.221 |
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Aviation stability analysis with coupled system criterion of theoretical solutions |
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C.C. Hung and T. Nguyễn
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| Abstract | ||
| In our research, we have proposed a solid solution for aviation analysis which can ensure the asymptotic stability of coupled nonlinear plants, according to the theoretical solutions and demonstrated method. Because this solution employed the scheme of specific novel theorem of control, the controllers are artificially combined by the parallel distribution computation to have a feasible solution given the random coupled systems with aviation stability analysis. Therefore, we empathize and manually derive the results which shows the utilized lemma and criterion are believed effective and efficient for aircraft structural analysis of composite and nonlinear scenarios. To be fair, the experiment by numerical computation and calculations were explained the perfectness of the methodology we provided in the research. | ||
| Key Words | ||
| aviation vehicles; inequality controlling & nonlinear stability analysis; linear matrix; spacecraft | ||
| Address | ||
| C.C. Hung: Faculty of National Hsin Hua Senior High School, Tainan, Taiwan T. Nguyễn: Ha Tinh University, Dai Nai Campus: No. 447, Street 26/3, Dai Nai Ward, Ha Tinh City, Vietnam | ||
