Study of Active Disturbance Rejection Control in Aero-Engine

Abstract:

The control problem of certain type of aero-engine is studied in the article. And active disturbance rejection control (ADRC) is applied into the control of aero-engine. In light of the problem of parameter optimization in ADRC, through the principle of parameter optimization analysis, rule of parameter optimization is revealed in this article. Based on parameter optimization rule, an adaptive parameter optimization law is designed to optimize the parameter of ADRC by on-line adaptive parameter tuning method. Some conclusions are suggested by the simulation result: compared with PID controller, that the ADRC controller is proved better in responding time, overshoot, steady-state error, disturbance rejection performance and control performance.

• Periodical: Applied Mechanics and Materials (Volume 344)
• Pages: 164-169
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.344.164
• Online since: July 2013
• Authors: Jiu Long Jiang, Xue Ren Li, Jun Du, Chen Wu
• Keywords: Active Disturbance Rejection Controller (ADRC), Adaptive Parameter Optimization, Aero-Engine, Online Optimization, Parameter Optimization

References

[1] XIE Shousheng. A certain afterburning turbofan engine[M]. Xian: AirForce Engineering University, (2002).

[2] SUN-Fengchen, SUN-Jianguo, ZHANGHaibo, Application of quantum genetic algorithm to aero-engine PID control systems. TOURNAL OF PROPULSDN TECHNOLOGY . Vo1. 28 No. 3. Jun. (2007).

[3] ZHANG Haibo, SUN JIanguo. Application of active disturbance rejection control method in aero-engines after-burning transition state control [J] . TOURNAL OF PROPULSDN TECHNOLOGY. Vo1. 31 No. 2 . Apr. (2010).

[4] YANG Ting ting, LI Aijun, HOU Zhen. An ADRC Flight Controller Design Method Based on PSO Algorithm[J]. Computer Simulation. Vol. 26. No. 9. 2009. 9.

[5] XIAO Yongli, ZHANG Chen. A kinds of the onlinear PID Algorithm for Position Servo systems[J]. Electrical Automation. No. 1, (2000).