Model-based Nonlinear Control of Aeroengines / by Jiqiang Wang, Weicun Zhang, Zhongzhi Hu
By: Wang, Jiqiang
Material type:
E-bookPublisher: Singapore : Springer International Publishing,, 2022Edition: 1st edition 2022.Description: 1 recurso en línea (XIX, 238 páginas) : 132 ilustraciones, 101 ilustraciones a color.ISBN: 9789811644535.Subject: Sistemas, Teoría de
| Item type | Current library | Collection | Call number | Status | Date due | Barcode | Item holds | |
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LIBRO-E NO PRÉSTAMO
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Madrid Digital Acceso Electrónico (UEM) | Ciencias e Ingeniería | QA402.35 .A383 2022 (Browse shelf(Opens below)) | Acceso electrónico | eBook.09012037 |
Introduction to Aeroengine Controls -- Aeroengine Nonlinear Modeling -- Model-based Aeroengine Nonlinear Set Point Control -- Model-based Aeroengine Nonlinear Transient Control -- Optimization-based Aeroengine Nonlinear Control Integration -- Conclusions & Further Development.
This book aims to develop systematic design methodologies to model-based nonlinear control of aeroengines, focusing on (1) modelling of aeroengine systems-both component-level and identification-based models will be extensively studied and compared; and (2) advanced nonlinear control designs-set-point control, transient control and limit-protection control approaches will all be investigated. The model-based design has been one of the pivotal technologies to advanced control and health management of propulsion systems. It can fulfil advanced designs such as fault-tolerant control, engine modes control and direct thrust control. As a consequence, model-based design has become an important research area in the field of aeroengines due to its theoretical interests and engineering significance. One of the central issues in model-based controls is the tackling of nonlinearities. There are publications concerning with either nonlinear modelling or nonlinear controls; yet, they are scattered throughout the literature. It is time to provide a comprehensive summary of model-based nonlinear controls. Consequently, a series of important results are obtained and a systematic design methodology is developed which provides consistently enhanced performance over a large flight/operational envelope, and it is thus expected to provide useful guidance to practical engineering in aeroengine industry and research. .
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