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Record Nr. |
UNINA9910743263303321 |
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Autore |
Wang Jiqiang |
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Titolo |
Model-based nonlinear control of aeroengines / / Jiqiang Wang, Weicun Zhang, Zhongzhi Hu |
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Pubbl/distr/stampa |
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Singapore : , : Springer, , [2021] |
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©2021 |
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ISBN |
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981-16-4453-5 |
981-16-4452-7 |
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Descrizione fisica |
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1 online resource (255 pages) : illustrations (some color) |
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Disciplina |
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Soggetti |
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Aerospace engineering |
Airplanes - Motors |
Nonlinear control theory |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Sommario/riassunto |
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This book aims to develop systematic design methodologies to model-based nonlinear control of aeroengines, focusing on (1) modelling of aeroengine systemsboth component-level and identification-based models will be extensively studied and compared; and (2) advanced nonlinear control designsset-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 |
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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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