A multi-input based full envelope acceleration schedule design method for gas turbine engine based on multilayer perceptron network

Author:

Wang KangORCID,Xu Maojun,Li MingORCID,Geng Jia,Liu Jinxin,Song Zhiping

Funder

National Natural Science Foundation of China

Ministry of Industry and Information Technology of the People's Republic of China

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. Aircraft Engine Controls: Design, System Analysis, and Health Monitoring;Jaw,2009

2. A modeling method for aero-engine by combining stochastic gradient descent with support vector regression;Ren;Aerosp. Sci. Technol.,2020

3. Application of the Tool for Turbine Engine Closed-Loop Transient Analysis (TTECTRA) for Dynamic Systems Analysis;Csank,2014

4. Life cycle gas path performance monitoring with control loop parameters uncertainty for aeroengine;Jin;Aerosp. Sci. Technol.,2021

5. Control Design for a Generic Commercial Aircraft Engine;Csank,2010

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