| Citation: | ZHENG Qiangang, JIN Chongwen, XIANG Dewei. Performance seeking control of aero-engine based on nonlinear model prediction[J]. Journal of Aerospace Power, 2023, 38（6）：1525-1536 doi: 10.13224/j.cnki.jasp.20210290
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To improve the response speed of aero-engine performance seeking control, an aero-engine performance seeking control method based on nonlinear model prediction control was proposed. The full envelope interpolation compact propulsion system dynamic model was used as the on-board model to estimate the engine performance parameters and the future outputs of the limited time domain. With the nonlinear model prediction control method, three typical performance seeking control modes, i.e.: the maximum thrust mode, the minimum fuel consumption mode and the minimum turbine temperature mode were changed into real-time performance seeking, and corresponding real-time control performance indexes were designed to improve engine response speed. The simulation results showed that compared with the traditional method, the proposed control method had better control effect under three performance optimization control modes, and the response speed increased from 0.5 s to 5 s. At the high altitude cruising working point the thrust of the maximum thrust mode increased by 19.8%; the fuel consumption rate of the minimum fuel consumption mode dropped by 3.12%; the temperature of the minimum turbine temperature mode dropped by 17 K, helping to verify the effectiveness of the control method.
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