民用航空发动机过渡状态变重SDRE控制算法设计

Q2 Engineering

CEAS Aeronautical Journal Pub Date : 2023-03-01 DOI:10.1007/s13272-023-00657-y

Han Zhenghong, Wang Wei, Liu Shuai, Bai Jie

引用次数: 0

摘要

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

Design of variable weight SDRE control algorithm for civil aeroengine transition state

求助全文

通过发布文献求助，成功后即可免费获取论文全文。去求助

来源期刊

CEAS Aeronautical Journal Engineering-Aerospace Engineering

CiteScore

3.40

自引率

0.00%

发文量

期刊介绍： The CEAS Aeronautical Journal has been created under the umbrella of CEAS to provide an appropriate platform for excellent scientific publications submitted by scientists and engineers. The German Aerospace Center (DLR) and the European Space Agency (ESA) support the Journal.The Journal is devoted to publishing results and findings in all areas of aeronautics-related science and technology as well as reports on new developments in design and manufacturing of aircraft, rotorcraft, and unmanned aerial vehicles. Of interest are also (invited) in-depth reviews of the status of development in specific areas of relevance to aeronautics, and descriptions of the potential way forward. Typical disciplines of interest include flight physics and aerodynamics, aeroelasticity and structural mechanics, aeroacoustics, structures and materials, flight mechanics and flight control, systems, flight guidance, air traffic management, communication, navigation and surveillance, aircraft and aircraft design, rotorcraft and propulsion.The Journal publishes peer-reviewed original articles, (invited) reviews and short communications.