Transition state performance optimization of propfan engine based on DDPG algorithm

As the “heart” of an aircraft, aero-engines work in harsh environments of high temperature and high pressure for a long time. In order to ensure that the engine can operate safely and reliably within the entire flight envelope, a large safety margin needs to be reserved in the design of the control...

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Vydané v:	Journal of physics. Conference series Ročník 2472; číslo 1; s. 12010 - 12015
Hlavní autori:	Zheng, Hua, Yang, Zhao-xing, Wang, Ya-fan, Zhao, Dong-zhu
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	Bristol IOP Publishing 01.05.2023
Predmet:	Aerospace engines Aircraft engines Algorithms Control systems design Flight envelopes High temperature Machine learning Optimization Physics Propfans Safety margins
ISSN:	1742-6588, 1742-6596
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