Research on an inlet-engine hybrid integrated modelling method with pressure dynamic self-tuning

Author:

Ouyang Tingyi,Liu Yi,Jin Zexi,Miao Huihui,Geng JiaORCID,Liu JinxinORCID,Ma Yuan,Song ZhipingORCID

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference52 articles.

1. Robust sensor fault detection and isolation of gas turbine engines subjected to time-varying parameter uncertainties;Pourbabaee;Mech. Syst. Signal Process.,2016

2. Uncertainties in gas-path diagnosis of gas turbines: Representation and impact analysis;Liao;Aerosp. Sci. Technol.,2021

3. A multi-input based full envelope acceleration schedule design method for gas turbine engine based on multilayer perceptron network;Wang;Aerosp. Sci. Technol.,2022

4. A highly robust thrust estimation method with dissimilar redundancy framework for gas turbine engine;Zhao;Energy,2022

5. Analysis of velocity and altitude characteristics at typical operating conditions based on control law of PATR engine (in Chinese);Ma;J. Rocket Propulsion,2022

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