A highly robust thrust estimation method with dissimilar redundancy framework for gas turbine engine

Author:

Zhao Hang,Liao ZengbuORCID,Liu Jinxin,Li Ming,Liu Wei,Wang Lei,Song Zhiping

Funder

National Natural Science Foundation of China

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

General Energy,Pollution,Mechanical Engineering,Building and Construction,Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Civil and Structural Engineering

Reference46 articles.

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3. On-board real-time optimization control for turbofan engine thrust under flight emergency condition;Zheng;Proc IME J Syst Control Eng,2017

4. HNN-based generalized predictive control for turbofan engine direct performance optimization;Zhou;Aero Sci Technol,2021

5. Turbojet direct-thrust control scheme for full-envelope fuel consumption minimization;Villarreal-Valderrama;Aircraft Eng Aero Technol,2021

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