Name: Model-Based Nonlinear Control of Aeroengines (en Inglés)
Price: 889003.00 COP
Availability: InStock
Author: Wang, Jiqiang ; Zhang, Weicun ; Hu, Zhongzhi
ISBN: 9789811644528

portada Model-Based Nonlinear Control of Aeroengines (en Inglés)

Formato

Libro Físico

Autor

Editorial

Idioma

Inglés

N° páginas

238

Encuadernación

Tapa Dura

Dimensiones

23.4 x 15.6 x 1.6 cm

Peso

0.54 kg.

ISBN13

9789811644528

Categorías

Ingeniería: general
Ingeniería de control automático
Tecnología aeroespacial y aeronáutica
Astronáutica

Model-Based Nonlinear Control of Aeroengines (en Inglés)

Weicun Zhang (Autor) · Jiqiang Wang (Autor) · Zhongzhi Hu (Autor) · Springer · Tapa Dura

Libro Físico

$ 889.003

$ 1.367.696

Ahorras: $ 478.694

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Envío normal

Origen: Estados Unidos (Costos de importación incluídos en el precio)

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Reseña del libro "Model-Based Nonlinear Control of Aeroengines (en Inglés)"

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.