This research work is supported by the National Science and Technology Major Project(2017-V-0004-0054);the National Natural Science Foundation of China(Grant No.52125603);the National Natural Science Foundation of China(Grant No.11972139);the Fundamental Research Funds for the Central Universities(HIT.BRET.2021006 and FRFCU5710094620).
Airbreathing aero-engines are regarded as excellent propulsion devices from ground takeoff to hypersonic flight,and require control systems to ensure their efficient and safe operation.Therefore,the present paper aims...