Predictive control method for mode transition process of multi-mode turbine engine based on onboard adaptive composite model

被引:1
|
作者
Cai, Changpeng [1 ]
Zheng, Qiangang [1 ]
Wang, Yong [1 ]
Chen, Haoying [1 ]
Zhang, Haibo [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China
关键词
Multi -mode turbine engine; Mode transition; Onboard adaptive model; Model predictive control;
D O I
10.1016/j.energy.2024.131748
中图分类号
O414.1 [热力学];
学科分类号
摘要
In order to achieve precise control of thrust and flow during the mode transition(MT) process of multi -mode turbine engine(MMTE) within the switching envelope and under the condition of engine performance degradation, research on multi -mode model predictive control method is conducted. A mode transition trajectory optimization method based on SQP is explored, and a small range of adjustable parameters that ensure the continuous thrust and flow is obtained. Based on this, a multi -mode onboard modeling approach based on the directional adjustment law scheduling of the variable geometry adjustment mechanism is proposed. Furthermore, an investigation into a predictive control method for MT process based on onboard adaptive composite model is conducted. The simulation results demonstrate that the proposed method exhibits a maximum thrust fluctuation of less than 0.66 % during MT process, under both normal and degraded engine component performance conditions, which is significantly superior to the conventional PID control of 2.8 %. Compared to the average single step calculation time of 7.24 ms using the SQP optimization method, the proposed approach only requires 0.204 ms. The methodology presented takes into consideration of control accuracy and computing efficiency, thereby offering promising prospects for engineering applications in MMTE MT control system design.
引用
收藏
页数:20
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