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008			210817s2022 si | s |||| 0|eng d
020			_a9789811644535
024	7		_a10.1007/978-981-16-4453-5 _2doi
040			_aES-MaUEC _bspa _cES-MaUEC _dES-MaUEC
050		4	_aQA402.35 A383 _b2022
100	1		_aWang, Jiqiang _9685922
245	1	0	_aModel-based Nonlinear Control of Aeroengines _cby Jiqiang Wang, Weicun Zhang, Zhongzhi Hu
250			_a1st edition 2022
264		1	_aSingapore _bSpringer International Publishing, _c2022
300			_a1 recurso en línea (XIX, 238 páginas) _b132 ilustraciones, 101 ilustraciones a color
336			_atexto _btxt _2rdacontent
337			_aelectrónico _bc _2rdamedia
338			_arecurso electrónico _bcr _2rdacarrier
347			_aarchivo de texto _bPDF
505	0		_aIntroduction 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.
520			_aThis 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. .
988			_aSpringer_Robotics_2022
650		7	_2embne _9141328 _aSistemas, Teoría de
776	0	8	_iPrinted edition: _z9789811644528
776	0	8	_iPrinted edition: _z9789811644542
776	0	8	_iPrinted edition: _z9789811644559
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-981-16-4453-5 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942			_2lcc _cLE
998			_b01/2023 _dz _eh _zSI