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Advances in Aircraft and Spacecraft Science Volume 10, Number 4, July 2023 , pages 369-391 DOI: https://doi.org/10.12989/aas.2023.10.4.369 |
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The nonlinear fuzzy intelligent theory for high-bypass-ratio two-spool unmixed-flow jet engines |
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C.C. Hung and T. Nguyen
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| Abstract | ||
| In our research we have offered a solid solution for aeronautical analysis. which can guarantee the asymptotic stability of coupled nonlinear facilities. According to the theoretical solutions and methods presented, the engine of this aircraft is a small high-bypass turbofan engine. using the non-linear aero-motor control approach and this paper focuses on the power management function of the aero-motor control system. These include static controls and transient controls. A mathematical model of the high-bypass-ratio two-spool unmixed-flow aeroengine was developed through a set of nonlinear dynamic equations verified by experimental data. A single actuator using the displacement method is designed to maintain a certain level of thrust under steady-state conditions. and maintains repeatable performance during transient operation from the requested thrust phase to the next. A single controller can compensate for the effects of noise and harmonic noise at many performance points. And the dynamic performance of a single controller is satisfactory during the transient. for fairness Numerical and computer experiments are described in the perfection of the methods we offer in 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. Nguyen: Ha Tinh University, Dai Nai Ward, Ha Tinh City, Vietnam | ||
