Volume 40 Issue 11
Nov.  2025
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ZHANG Yuzhu, ZHOU Xin, CHEN Wenjuan, et al. ACE thrust maintenance method based on model free adaptive control[J]. Journal of Aerospace Power, 2025, 40(11):20230766 doi: 10.13224/j.cnki.jasp.20230766
Citation: ZHANG Yuzhu, ZHOU Xin, CHEN Wenjuan, et al. ACE thrust maintenance method based on model free adaptive control[J]. Journal of Aerospace Power, 2025, 40(11):20230766 doi: 10.13224/j.cnki.jasp.20230766

ACE thrust maintenance method based on model free adaptive control

doi: 10.13224/j.cnki.jasp.20230766
  • Received Date: 2023-12-04
    Available Online: 2025-08-12
  • Adaptive cycle engine (ACE) has strong nonlinear characteristics and severe coupling between parameters. It is difficult to establish high-precision mathematical models. The model free adaptive control (MFAC) algorithm was employed to design a controller by dynamically linearizing its input/output (I/O) data without an accurate model of the controlled object. This algorithm had low computational burden and strong robustness. A multivariable model free adaptive control strategy for ACE single mode was designed based on a certain adaptive cycle engine. By introducing an integral part, the fluctuation of control variables and the dynamic performance of the system were improved. Regarding the thrust maintenance control problem of ACE, artificial bee colony (ABC) optimization algorithm and PID-linear programming (PID-LP) comprehensive optimization algorithm were proposed to design an outer loop instruction correction loop. A dual loop multivariable control system was constructed to control the turbine temperature and compressor surge margin within the limit boundary while maintaining engine thrust. Hardware in-loop simulation tests were conducted. The simulation results demonstrated that the improved MFAC dual-loop thrust control structure enabled the engine to achieve excellent steady-state and dynamic control performance. The fluctuation of the controlled variable remained below 2%, and thrust maintenance within safe limits can be achieved even under conditions of deteriorating gas path component performance. This approach optimized engine performance, extended engine service life, and exhibited significant engineering application value.

     

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