Active disturbance rejection control method of auxiliary power unit

被引：0

作者：

Qiu X. ^{[1
]}

Zhang Y. ^{[1
]}

Li Y. ^{[1
]}

机构：

[1] Aero Engine Control System Institute, Aero Engine Corporation of China, Jiangsu, Wuxi

来源：

Hangkong Dongli Xuebao/Journal of Aerospace Power | 2024年 / 39卷 / 02期

关键词：

active disturbance rejection control; auxiliary power unit; control system; parametric design method; PI control;

D O I：

10.13224/j.cnki.jasp.20220035

中图分类号：

学科分类号：

摘要：

The auxiliary power unit is often used to extract shaft power and air flow for power generation and bleed. In order to reduce the interference caused by this process to the turbine engine and improve the anti-interference performance of the original control system, the active disturbance rejection control method and its parametric design method were studied, so as to design the corresponding control parameters according to the linearization model in engineering applications, and numerical simulation of a factory model based on the traditional gain scheduling PI control method and active disturbance rejection control (ADRC) method was conducted. Results showed that, on the premise of keeping the basic performance similar to that of PI control, ADRC had good anti-power generation interference and air entrainment interference performance, and can recover to the original working state faster when the interference occurred. More specifically, the speed fluctuation of ADRC was reduced by 35%, and the speed adjustment time was shortened by 9%, revealing the superior potential for practical engineering applications. © 2024 BUAA Press. All rights reserved.

引用

共 18 条

[1]

LIN Kun, Discuss future trends of APU from the comparison of three models APU, Popular Science & Technology, 15, 1, pp. 53-54, (2013)

[2]

ZHANG Ying, Research on full authority digital electronic control system of the auxiliary power unit, (2007)

[3]

LI Dongjie, Application status and development trend of auxiliary power unit, Aeronautical Science & Technology, 23, 6, pp. 7-10, (2012)

[4]

XU Jian, YANG Gang, HU Wenfei, Research on applying root locus to parameter design of fuel control loop PI controller, Aeroengine, 42, 4, pp. 17-20, (2016)

[5]

ZILOUCHIAN A, JULIANO M, HEALY T, Et al., Design of a fuzzy logic controller for a jet engine fuel system, Control Engineering Practice, 8, 8, pp. 873-883, (2000)

[6]

QIU Xiaojie, LIN Xingchen, WANG Quansheng, Et al., Research of speed overshoot control technology in high altitude for missile engine control systems, Aeroengine, 44, 3, pp. 31-35, (2018)

[7]

WANG C, LI Y G, YANG B Y., Transient performance simulation of aircraft engine integrated with fuel and control systems, Applied Thermal Engineering, 114, pp. 1029-1037, (2017)

[8]

TSOUTSANIS E, MESKIN N., Performance assessment of classical and fractional controllers for transient operation of gas turbine engines, IFAC-PapersOnLine, 51, 4, pp. 687-692, (2018)

[9]

CUI Tao, Simplified procedure for controlling pressure distribution of a scramjet combustor, Chinese Journal of Aeronautics, 27, 5, pp. 1137-1141, (2014)

[10]

(2014)

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