Test Simulation and Control Law Optimization of Micro-Turbojet Engines

A comprehensive testing plan was designed for the micro turbojet engine, and the overall performance simulation model was corrected using steady-state test data. Then, the corrected model was successfully simulated and fitted with the experimental transient data. Based on the corrected model, the di...

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Bibliographic Details
Published in2023 14th International Conference on Mechanical and Aerospace Engineering (ICMAE) pp. 144 - 150
Main Authors Liu, Zhen, Jia, Lin-Yuan, Wang, Han-Yang, Zhao, Zhen-Nan, Kong, Fan-Qi, Wang, Yu-Ru
Format Conference Proceeding
LanguageEnglish
Published IEEE 18.07.2023
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Summary:A comprehensive testing plan was designed for the micro turbojet engine, and the overall performance simulation model was corrected using steady-state test data. Then, the corrected model was successfully simulated and fitted with the experimental transient data. Based on the corrected model, the differential evolution algorithm was used to optimize the PID parameters in the acceleration and deceleration control law.
DOI:10.1109/ICMAE59650.2023.10424640