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Coordinated control of fuel flow rate and air flow rate of a supersonic heat-airflow simulated test system

Published online by Cambridge University Press:  19 March 2020

C. Cai Open the ORCID record for C. Cai [Opens in a new window] ,
L. Guo  and
J. Liu
C. Cai*
Affiliation:
School of Mechanical and Equipment Engineering, Hebei University of Engineering, Handan, Hebei, China
L. Guo
Affiliation:
School of Mechanical and Equipment Engineering, Hebei University of Engineering, Handan, Hebei, China
J. Liu
Affiliation:
School of Mechanical and Equipment Engineering, Hebei University of Engineering, Handan, Hebei, China
*
caichaozhi1983@163.com
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Abstract

The gas temperature of the supersonic heat airflow simulated test system is mainly determined by the fuel and air flow rates which enter the system combustor. In order to realise a high-quality control of gas temperature, in addition to maintaining the optimum ratio of fuel and air flow rates, the dynamic characteristics of them in the combustion process are also required to be synchronised. Aiming at the coordinated control problem of fuel and air flow rates, the mathematical models of fuel and air supply subsystems are established, and the characteristics of the systems are analysed. According to the characteristics of the systems and the requirements of coordinated control, a fuzzy-PI cross-coupling coordinated control strategy based on neural sliding mode predictive control is proposed. On this basis, the proposed control algorithm is simulated and experimentally studied. The results show that the proposed control algorithm has good control performance. It cannot only realise the accurate control of fuel flow rate and air flow rate, but also realise the coordinated control of the two.

Keywords

Supersonicfuel flow rateair flow rateneural sliding mode predictive controlcoordinated control
Type
Research Article
Information
The Aeronautical Journal , Volume 124 , Issue 1278 , August 2020 , pp. 1170 - 1189
Copyright
© The Author(s) 2020. Published by Cambridge University Press on behalf of Royal Aeronautical Society

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